Best Paper – Propulsion and Energy Group
Best Papers in a specific propulsion or energy discipline are selected from papers presented at technical forums by the respective technical committee.
Award Recipients
2025
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Dr Troy HendersonEmbry-Riddle Aeronautical UniversityAwardedAward: 2024 AIAA Aerospace Power Systems Best Student PaperAIAA Citation: Power System Testing and Verification for a Space Camera System With 18650 Batteries AIAA 2024-0021
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Prof Christopher S GoldensteinPurdue UniversityAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Dr Vivek AhujaRESEARCH IN FLIGHTAwardedAward: 2023 AIAA Solid Rockets Best Student Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics Using a Vortex Particle Method AIAA 2023-4032
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Mr Chris N TorreTorre Space and Power SystemsAwardedAward: 2024 AIAA Aerospace Power Systems Best PaperAIAA Citation: Test Performance Results of a Magnetohydrodynamic Generator System Using an Ionized Plasma Flow to Simulate the Interplanetary Solar Wind AIAA 2024-0472
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Roy J Hartfield JrAuburn UniversityAwardedAward: 2023 AIAA Solid Rockets Best Student Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics Using a Vortex Particle Method AIAA 2023-4032
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Vishnu RadhakrishnaSandia National LaboratoriesAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Kyle E UhlenhakePurdue UniversityAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
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Griffin A DiMaggioAwardedAward: 2023 AIAA Solid Rockets Best Student Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics Using a Vortex Particle Method AIAA 2023-4032
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William V TorreTorre Space and Power Systems LLCAwardedAward: 2024 AIAA Aerospace Power Systems Best PaperAIAA Citation: Test Performance Results of a Magnetohydrodynamic Generator System Using an Ionized Plasma Flow to Simulate the Interplanetary Solar Wind AIAA 2024-0472
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Daniel PosadaEmbry-Riddle Aeronautical UniversityAwardedAward: 2024 AIAA Aerospace Power Systems Best Student PaperAIAA Citation: Power System Testing and Verification for a Space Camera System With 18650 Batteries AIAA 2024-0021
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Prof Steven F SonPurdue UniversityAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Dual-Zone Temperature and Multi-Species Measurements in Solid-Propellant Flames via Broadband Mid-Infrared Laser Absorption Spectroscopy AIAA 2023-4029
2024
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Dr Eric BachPurdue UniversityAwardedAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Dr Leanne L SuUniversity of MichiganAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Thomas A MarksUniversity of Michigan, Ann ArborAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Parker J RobertsUniversity of Michigan, Ann ArborAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Stefano DossiPolitecnico Di MilanoAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Mr Eric VigesUniversity of Michigan, Ann ArborAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Spencer L StahlAwardedAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Dr John T SpyropoulosNAVAIRAwardedAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Prof Christian O PaschereitTechnische Universität BerlinAwardedAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Marco AdornoPolitecnico di TorinoAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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William HurleyUniversity of MichiganAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Collin B WhittakerUniversity of MichiganAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Dr Christopher R MarksAir Force Research LaboratoryAwardedAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Dr Mitch WolffWright State UniversityAwardedAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Dr Filippo MaggiPolitecnico Di MilanoAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Andrea GalavottiSPLabAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Jan MartinDLRAwardedAward: 2023 AIAA Liquid Propulsion Best PaperAIAA Citation: Flame-Acoustic Interaction in a Sub- and Supercritical, Single-Injector, LOX/CNG/LNG Rocket Combustor with Optical Access AIAA 2023-1838
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Esteban Cisneros-GaribayPrinceton UniversityAwardedAward: 2023 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: Manifold-based Modeling for Supersonic Turbulent Combustion AIAA 2023-2529
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Madison G AllenNAAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Jared N KerestesWright State UniversityAwardedAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Dr John P ClarkAFRLAwardedAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Nathan FletcherInnovative Scientific Solutions, Inc.AwardedAward: 2023 AIAA Gas Turbine Engines Best PaperAIAA Citation: High-Lift High-Work LPT Blades and Separation: A Machine-Learning-Based Approach to Separation Identification AIAA 2023-0113
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Tate GillUniversity of Michigan, Ann ArborAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Dr Stefania CarlottiPolitecnico di MilanoAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Justin HardiDLR Institute of Space PropulsionAwardedAward: 2023 AIAA Liquid Propulsion Best PaperAIAA Citation: Flame-Acoustic Interaction in a Sub- and Supercritical, Single-Injector, LOX/CNG/LNG Rocket Combustor with Optical Access AIAA 2023-1838
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Mr Matthew ByrnePEPLAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Mr Luca NicheliniPolitecnico di MilanoAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Myles BohonTechnische Universität BerlinAwardedAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Mr Wolfgang ArmbrusterDLR-German Aerospace CenterAwardedAward: 2023 AIAA Liquid Propulsion Best PaperAIAA Citation: Flame-Acoustic Interaction in a Sub- and Supercritical, Single-Injector, LOX/CNG/LNG Rocket Combustor with Optical Access AIAA 2023-1838
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Prof Ephraim J GutmarkUniversity of CincinnatiAwardedAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
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Dr Arianna MasiniHomeAwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Dr Datta V GaitondeThe Ohio State UniversityAwardedAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Dr Russell W PowersNaval Air Warfare CenterAwardedAward: 2023 AIAA Inlets, Nozzles, and Propulsion System Integration Best PaperAIAA Citation: Modal Analysis of Serpentine Diffuser Distortion AIAA 2023-3308
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Mr Christopher L SercelAwardedAward: 2023 AIAA Electric Propulsion Best PaperAIAA Citation: Operation and Performance of a Magnetically Shielded Hall Thruster at Ultrahigh Current Densities on Xenon and Krypton AIAA 2023-0842
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Dr Agostino NeriEuropean Space Agency (ESA)AwardedAward: 2023 AIAA Solid Rockets Best PaperAIAA Citation: Quantification of HCl in Solid Propellant Combustion Products AIAA 2023-1515
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Miss Provence BarnouinTU BerlinAwardedAward: 2023 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors AIAA 2023-1291
2023
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Mr Koichi MatsuyamaIMaSS, Nagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Prof Daniele BianchiSapienza University of RomeAwardedAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Prof Hiroto HabuJapan Aerospace Exploration AgencyAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Hiroaki WatanabeCRIEPIAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Qili LiuPurdue UniversityAwardedAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Dr Noboru ItouyamaNagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Mark P WernetNASA Glenn Research CenterAwardedAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Parker J RobertsUniversity of Michigan, Ann ArborAwardedAward: 2022 AIAA Electric Propulsion Best PaperAIAA Citation: Experimental Characterization of Wave-Induced Azimuthal Ion Velocities in a Hollow Cathode Plume AIAA 2022-1561
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Dr Mirko GambaUniversity of MichiganAwardedAward: 2021 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Effects of Inlet Area Ratio on Operability of an Axial Air Inlet Rotating Detonation Combustor AIAA 2021-3676
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Prof Li QiaoSchool of Aeronautics & Astronautics, Purdue UniversityAwardedAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Ms Carolyn WoeberCadence Design Systems, Inc.AwardedAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Joshua ShepardUniversity of MichiganAwardedAward: 2021 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Effects of Inlet Area Ratio on Operability of an Axial Air Inlet Rotating Detonation Combustor AIAA 2021-3676
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Dr Masaharu UchiumiJapan Aerospace Exploration AgencyAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Paolo Maria ZollaLa SapienzaAwardedAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Akira KawasakiAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Brian T BojkoNaval Research LaboratoryAwardedAward: 2021 AIAA Propellants and Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates AIAA 2021-1970
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Dr Shinsuke TakeuchiJapan Aerospace Exploration AgencyAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Fabio A BendanaAwardedAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Dr Benjamin L Emerson IIGeorgia Institute of TechnologyAwardedAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Dr Kazuhiko YamadaJapan Aerospace Exploration AgencyAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Chad M WinklerThe Boeing CompanyAwardedAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: 2022 AIAA Electric Propulsion Best PaperAIAA Citation: Experimental Characterization of Wave-Induced Azimuthal Ion Velocities in a Hollow Cathode Plume AIAA 2022-1561
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Simon RayAwardedAward: 2021 AIAA Propellants and Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates - AIAA 2021-1970
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Dr Ikkoh FunakiJapan Aerospace Exploration AgencyAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Raghul Manosh KumarGeorgia Institute of TechnologyAwardedAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Mr Lorenzo FedericiThe University of ArizonaAwardedAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Keisuke GotoNagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Monique McClainPurdue UniversityAwardedAward: 2021 AIAA Propellants and Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates AIAA 2021-1970
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Mr Kyungrae KangSeoul National UniversityAwardedAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Linkai LiNAUUAwardedAward: 2022 AIAA Gas Turbine Engine Best PaperAIAA Citation: An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model - AIAA 2022-2435
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Dr Nicholas J GeorgiadisNASA Glenn Research CenterAwardedAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Dr Linchuan TianAwardedAward: 2022 AIAA Gas Turbine Engine Best PaperAIAA Citation: An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model - AIAA 2022-2435
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Lt Col Darrell S CroweAir Force Institute of TechnologyAwardedAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Ms Isabelle C SandersUCLAAwardedAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Alexander FeleoGE AerospaceAwardedAward: 2021 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Effects of Inlet Area Ratio on Operability of an Axial Air Inlet Rotating Detonation Combustor AIAA 2021-3676
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Prof Hyungrok DoSeoul National UniversityAwardedAward: 2022 AIAA High Speed Air Breathing Propulsion Best PaperAIAA Citation: From Thermal Choking to Inlet Buzz of Circular Scramjets in High-Enthalpy Flows AIAA 2022-0202
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Dr Alessandro ZavoliSapienza University of RomeAwardedAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Subodh AdhikariAwardedAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Dr Vernon H ChaplinJet Propulsion Laboratory (JPL)AwardedAward: 2022 AIAA Electric Propulsion Best PaperAIAA Citation: Experimental Characterization of Wave-Induced Azimuthal Ion Velocities in a Hollow Cathode Plume AIAA 2022-1561
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Dr Daisuke NakataMuroran Institute of TechnologyAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Nora G. StacyUniversity of California Los AngelesAwardedAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Mr Kazuki IshiharaNagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Kristen Karman-ShoemakeCadence Design Systems, Inc.AwardedAward: 2022 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Summary of the 5th Propulsion Aerodynamics Workshop Nozzle Test Case: Heated Nozzle Exhaust Passing Over a Flim-cooled Plate AIAA 2022-0086
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Mr Tatsuro NakaoJapan Aerospace Exploration Agency (JAXA))AwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Christopher Allen FuggerSpectral Energies, LLCAwardedAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
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Mr Kevin SchwarmUCLAAwardedAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Valentin BuyakofuNagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Dr Mario Tindaro MigliorinoSapienza University of RomeAwardedAward: 2021 AIAA Hybrid Rockets Best PaperAIAA Citation: Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA 2021-3506
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Dr Raymond Mitchell SpearrinUniversity of California Los AngelesAwardedAward: 2021 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Swirl injection in hybrid PMMA combustion assessed by thermochemical imaging AIAA 2021-3513
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Prof Ken MatsuokaNagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Prof Steven F SonPurdue UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Modeling of Layered Ammonium Perchlorate Composite Propellant with Different Burning Rates - AIAA 2021-1970
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Prof Tim C LieuwenGeorgia Institute of TechnologyAwardedAward: 2022 AIAA Joint Liquid Propulsion and Propellants and Combustion Best Paper AwardAIAA Citation: Simultaneous OH, CH2O and flow field imaging of near blowoff dynamics AIAA-2022-2348
2022
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Daniel D LeeAwardedAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Dr Steven J SchneiderNASA Glenn Research CenterAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Prof Matteo BernardiniSapienza University of RomeAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Dr Francesco SalvadoreCINECAAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Mr. Andrea Di MascioINSEANAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Robin OrthUSAFAwardedAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Dr Vivek AhujaRESEARCH IN FLIGHTAwardedAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Dr Mirko GambaUniversity of MichiganAwardedAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Alicia Benhidjeb-CarayonBlue Origin LLCAwardedAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Dr Aaron H AuslenderNASA Langley Research CenterAwardedAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Robert P ThackerNASA Glenn Research CenterAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Dr Emanuele MartelliSecond University of NaplesAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Roy J Hartfield JrAuburn UniversityAwardedAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Dr Stephen A DanczykAFRL - Air Force Research LaboratoryAwardedAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Mr Zachary J FrederickNASA Langley Research CenterAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Kristyn JohnsonNational Energy Technology LaboratoryAwardedAward: 2021 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: Individual Wave Detection and Tracking within a Rotating Detonation Engine through Computer Vision Object Detection applied to High-Speed Images AIAA-2021-1382
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Daniel I PinedaAwardedAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Mark D GuynnNASA Langley Research CenterAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Mr Peter C FredericAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Joshua M WoodsUniversity of MichiganAwardedAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Dr Andrew C NixWest Virginia UniversityAwardedAward: 2021 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: Individual Wave Detection and Tracking within a Rotating Detonation Engine through Computer Vision Object Detection applied to High-Speed Images AIAA-2021-1382
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Anil P NairUniversity of California - Los AngelesAwardedAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Prof Fulvio StellaSapienza University of RomeAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Dr Jason Michael KrieselOpto-Knowledge Systems IncAwardedAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Dr William A Hargus JrAir Force Research LaboratoryAwardedAward: 2020 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: MHz Mid-infrared Laser Absorption of CO and CO2 for Pressure, Temperature, and Species in Rotating Detonation Rocket Flows AIAA-2020-3867
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Dr Nathaniel J BlaesserNASA Langley Research CenterAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Dr Louis M EdelmanNASA Langley Research CenterAwardedAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Tate GillUniversity of Michigan, Ann ArborAwardedAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Prof Jiro KasaharaNagoya UniversityAwardedAward: 2022 AIAA Pressure Gain Combustion Best PaperAIAA Citation: Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine AIAA 2022-0232
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Jason KirkNASA Langley Research CenterAwardedAward: 1AIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Dr Enrico CavalliniAgenzia Spaziale ItalianaAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Griffin A DiMaggioAwardedAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Mr Matteo CiminiSapienza University of RomeAwardedAward: 2021 AIAA Solid Rockets Best Paper AwardAIAA Citation: Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method AIAA-2021-3696
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Dr Jeffrey M DonbarUSAFAwardedAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Mr Jason R GablAwardedAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Dr Donald H FergusonNational Energy Technology LaboratoryAwardedAward: 2021 AIAA Pressure Gain Combustion Best Paper AwardAIAA Citation: Individual Wave Detection and Tracking within a Rotating Detonation Engine through Computer Vision Object Detection applied to High-Speed Images AIAA-2021-1382
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Victoria M BoulosAwardedAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Prof Joseph MajdalaniAuburn UniversityAwardedAward: 2022 AIAA Solid Rockets Best Paper AwardAIAA Citation: Solid Rocket Motor Internal Ballistics with a Surface-Vorticity Solver AIAA-2022-1898
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Ms Catriona WhitePurdue UniversityAwardedAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Dr Timothee L PourpointPurdue UniversityAwardedAward: 2021 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: Chemical Composition of Mixed Oxides of Nitrogen using Raman Spectroscopy AIAA-2021-3589
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Kenneth L FisherNASA-Glenn Research CenterAwardedAward: 2021 AIAA Electrified Aircraft Technology Best Paper AwardAIAA Citation: Results for an Electrified Aircraft Propulsion Design Exploration AIAA-2021-3280
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Mark A HagenmaierAir Force Reseach LaboratoryAwardedAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
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Mr Christopher L SercelAwardedAward: 2021 AIAA Electric Propulsion Best Paper AwardAIAA Citation: Performance Measurements of a 5 kW-Class Rotating Magnetic Field Thruster AIAA 2021-3384
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Dr Haiyang HuUniversity of Alabama, HuntsvilleAwardedAward: 2022 AIAA Gas Turbine Engine Best PaperAIAA Citation: An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model - AIAA 2022-2435
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Robin HuntNASA Langley Research CenterAwardedAward: 2021 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Application of Flux-Conserved Modeling to an Unsteady Combustion Driven Pseudo-Shock AIAA-2021-1763
2021
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Dr Elizabeth T JensJet Propulsion Laboratory (JPL)AwardedAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Prof Claude Russell Joyner IIL3HarrisAwardedAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Dr Eric BachPurdue UniversityAwardedAward: 2020 AIAA Pressure Gain Combustion Best Professional PaperAIAA Citation: RDC Operation and Performance with Varying Air Injector Pressure Loss (AIAA-2020-0199)
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Dr Qili LiuPurdue UniversityAwardedAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5 (AIAA-2020-1611)
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John C FikesFD02AwardedAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Paul R GradlNASA Marshall Space Flight CenterAwardedAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Mr Thomas A MarksUniversity of Michigan, Ann ArborAwardedAward: 2020 AIAA Electric Propulsion Best PaperAIAA Citation: A Predictive Hall Thruster Model Enabled by Data-Driven Closure AIAA-2020-3622
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Jason T CassibryUniversity of Alabama HuntsvilleAwardedAward: 2020 AIAA Power and Energy Forum Best Student PaperAIAA Citation: Elements of an Inductive Electrical Power Conversion System for Fusion-Class Plasmas AIAA-2020-3539
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Mr Brian J MuzekL3Harris TechnologiesAwardedAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Mr. Sandi G MillerNASA Glenn Research CenterAwardedAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Mr Mehmet KahramanDeltaV Space TechnologiesAwardedAward: 2020 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector AIAA-2020-3733
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Dr Timothy S KokanL3HarrisAwardedAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Dr Xavier CarbonneauISAE SUPAEROAwardedAward: 2021 AIAA Gas Turbine Engines Best PaperAIAA Citation: Unsteady Body Force Methodology for Fan Operability Assessment under Clean and Distorted Inflow Conditions AIAA-2021-0388
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Dr Lien C YangL Yang ConsultingAwardedAward: 2020 AIAA Energetic Components and Systems Best PaperAIAA Citation: New Formulation for Studying of Detonation Of Gaseous Energetic Mixtures II: CH4/O2 & CH4/Air AIAA-2020-3653
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Mr Joseph Kalyan Raj I.TECHNION - ISRAEL INST OF TECHAwardedAward: 2020 Power and Energy Forum Best Student PaperAIAA Citation: Development of a Deep Space Nuclear Electric Propulsion (NEP) System - a NuAER Plasma NEP Reactor AIAA-2020-3540
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Mr amaury AWESISAE SupaeroAwardedAward: 2021 AIAA Gas Turbine Engines Best PaperAIAA Citation: Unsteady Body Force Methodology for Fan Operability Assessment under Clean and Distorted Inflow Conditions AIAA-2021-0388
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Dr Robert B AdamsNASA Marshall Space Flight CenterAwardedAward: 2020 AIAA Power and Energy Forum Best Student PaperAIAA Citation: Elements of an Inductive Electrical Power Conversion System for Fusion-Class Plasmas AIAA-2020-3539
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Dr Arif M KarabeyogluSpace Propulsion Group, Inc.AwardedAward: 2020 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector AIAA-2020-3733
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Prof Christian O PaschereitTechnische Universität BerlinAwardedAward: 2020 AIAA Pressure Gain Combustion Best Professional PaperAIAA Citation: RDC Operation and Performance with Varying Air Injector Pressure Loss (AIAA-2020-0199)
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Dr Tonghun LeeUniversity of Illinois at Urbana ChampaignAwardedAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5 (AIAA-2020-1611)
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Mr George R WhittinghillWhittinghill Aerospace LLCAwardedAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: 2020 AIAA Electric Propulsion Best PaperAIAA Citation: A Predictive Hall Thruster Model Enabled by Data-Driven Closure AIAA-2020-3622
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Mr Christopher Britton ReynoldsL3HarrisAwardedAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Prof Panagiotis StathopoulosAwardedAward: 2020 AIAA Pressure Gain Combustion Best Professional PaperAIAA Citation: RDC Operation and Performance with Varying Air Injector Pressure Loss: (AIAA-2020-0199)
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Dr Julien MartyONERAAwardedAward: 2021 AIAA Gas Turbine Engines Best PaperAIAA Citation: Unsteady Body Force Methodology for Fan Operability Assessment under Clean and Distorted Inflow Conditions AIAA-2021-0388
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Dr Ashley C KarpJet Propulsion Laboratory (JPL)AwardedAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Matt Wentzel-LongNASA Glenn Research CenterAwardedAward: 2020 AIAA Power and Energy Forum Best PaperAIAA Citation: 2020 Propulsion and Energy Forum Power Generation from Interplanetary and Interstellar Plasma and Magnetic Fields
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Christopher S ProtzNASA Marshall Space Flight CenterAwardedAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Dr Mario KobaldHyImpulse Technologies GmbHAwardedAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Dr Gyu Sub LeeNoneAwardedAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5 (AIAA-2020-1611)
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Nathan SchillingAwardedAward: 2020 AIAA Power and Energy Forum Best Student PaperAIAA Citation: Elements of an Inductive Electrical Power Conversion System for Fusion-Class Plasmas AIAA-2020-3539
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Dr Gregory J HuntWilliam & MaryAwardedAward: 2020 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information AIAA-2020-3715
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Dr Martin SiggelDLR - German Aerospace CenterAwardedAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Dr Tyler B HudsonNASA Langley Research CenterAwardedAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Dr Alexander RüttgersGerman Aerospace Center (DLR)AwardedAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Mr Michael K LieuMORSE CorporationAwardedAward: 2021 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Propulsor Models for Computational Analysis of Aircraft Aerodynamic Performance with Boundary Layer Ingestion AIAA-2021-0991
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Dr Ethan Thomas DaleThe Aerospace CorporationAwardedAward: 2020 AIAA Electric Propulsion Best PaperAIAA Citation: A Predictive Hall Thruster Model Enabled by Data-Driven Closure AIAA-2020-3622
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Ms Anna PetraroloDLR LampoldshausenAwardedAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
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Mr. Ibrahim OzkalIstanbul Techinal UniversityAwardedAward: 2020 AIAA Hybrid Rockets Best Student PaperAIAA Citation: Enhancement of Fuel Regression Rate for Hybrid Rockets by Introducing Novel Coaxial Tube Injector AIAA-2020-3733
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Dr Damiano BaccarellaUniversity of TennesseeAwardedAward: 2020 AIAA High Speed Air Breathing Propulsion Best Professional PaperAIAA Citation: Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5 (AIAA-2020-1611)
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Prof David Kenneth HallThe Pennsylvania State UniversityAwardedAward: 2021 AIAA Inlets Nozzles and Propulsion System Integration Best PaperAIAA Citation: Propulsor Models for Computational Analysis of Aircraft Aerodynamic Performance with Boundary Layer Ingestion AIAA-2021-0991
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ENS David L EllisNASA Glenn Research CenterAwardedAward: 2020 AIAA Liquid Propulsion Best PaperAIAA Citation: Lightweight Thrust Chamber Assemblies using Multi-Alloy Additive Manufacturing and Composite Overwrap AIAA-2020-3787
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Dr Geoff ParksAwardedAward: 2020 Power and Energy Forum Best Student PaperAIAA Citation: Development of a Deep Space Nuclear Electric Propulsion (NEP) System - a NuAER Plasma NEP Reactor AIAA-2020-3540
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George T StoryNASA Marshall Space Flight CenterAwardedAward: 2020 AIAA Hybrid Rockets Best PaperAIAA Citation: Combustion Efficiency in Single Port Hybrid Rocket Engines AIAA-2020-3746
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Daniel J LevackL3HarrisAwardedAward: 2020 Nuclear and Future Flight Propulsion Best PaperAIAA Citation: Mars Opposition Missions Using Nuclear Thermal Propulsion AIAA-2020-3850
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Robin HuntNASA Langley Research CenterAwardedAward: 2020 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information AIAA-2020-3715
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Dr Geoffrey A LandisNASA Glenn Research CenterAwardedAward: 2020 AIAA Power and Energy Forum Best PaperAIAA Citation: 2020 Propulsion and Energy Forum Power Generation from Interplanetary and Interstellar Plasma and Magnetic Fields
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Dr Charlotte DebusDLR - German Aerospace CenterAwardedAward: 2020 AIAA Propellants and Combustion Best PaperAIAA Citation: High-performance data analytics of hybrid rocket fuel combustion data using different machine learning approaches AIAA-2020-1161
2020
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Prof Claude Russell Joyner IIL3HarrisAwardedAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Eur Ing Francesco Baratouniversità degli studi di PadovaAwardedAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Dr Christopher S ProtzNASAAwardedAward: 2019 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: “Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys” (AIAA-2019-4362)
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Dr Christopher S ProtzNASAAwardedAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Paul R GradlNASA Marshall Space Flight CenterAwardedAward: 2019 AIAA Liquid Propulsion Best PaperAIAA Citation: “Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys” (AIAA-2019-4362)
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Paul R GradlNASA Marshall Space Flight CenterAwardedAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Dr Andreea BocaJet Propulsion Laboratory (JPL)AwardedAward: 2019 AIAA Aerospace Power Systems Best Paper AwardAIAA Citation: “Solar Power for Deep-Space Applications: State of Art and Development” (AIAA 2019-4236)
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Daniele PavarinUniversity of PadovaAwardedAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Dr Kenneth A BrownSandia National LaboratoriesAwardedAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper Award fromAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Jeffrey D MoorePenn State AltoonaAwardedAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Mr Cory CombsAmpaire Inc.AwardedAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwardAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Flora S MechentelJet Propulsion Laboratory (JPL)AwardedAward: 2019 AIAA Hybrid Rockets Best Student Paper AwardAIAA Citation: “Experimental Findings on Pre- and Post-combustion Chamber Effects in a Laboratory-scale motor” (AIAA 2019-4336)
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Dr Ali A AmeriNASA Glenn Research CenterAwardedAward: 2020 AIAA Gas Turbine Engines Best Paper AwardAIAA Citation: “Conjugate Heat Transfer Study of Innovative Pin-Fin Cooling Configuration ” (AIAA-2020-0634)
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Dr Timothy S KokanL3HarrisAwardedAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Mr Austin P MurrayAwardedAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Tal WammenNASA Marshall Space Flight CenterAwardedAward: 2019 AIAA Liquid Propulsion Best Paper AwardAIAA Citation: “Additive Manufacturing and Hot-fire Testing of Liquid Rocket Channel Wall Nozzles Using Blown Powder Directed Energy Deposition Inconel 625 and JBK-75 Alloys” (AIAA-2019-4362)
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Robert S KowalczykAwardedAward: 2019 AIAA Aerospace Power Systems Best Paper AwardAIAA Citation: “Solar Power for Deep-Space Applications: State of Art and Development” (AIAA 2019-4236)
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Patrick McClureLos Alamos National LaboratoryAwardedAward: 2019 AIAA Aerospace Power Systems Best Student Paper Competition AwardAIAA Citation: “Hydrogen Loss Effects on Mircoreactors for Space and Planetary Nuclear Power Production” (AIAA 2019-4452)
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Brandon RobertsAwardedAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Laura EvansNASA Glenn Research CenterAwardedAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Mr Matthew D LangfordTechsburg, Inc.AwardedAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwaAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Cody Ryan GroundNASA Langley Research CenterAwardedAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Mr John A Brand IILeidosAwardedAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Mr Tyler L Smith IAwardedAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Kennethe G CooperNASA Marshall Space Flight CenterAwardedAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Marco SantiPrivate residenceAwardedAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Mr Enrico PaccagnellaAwardedAward: 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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Mr Ashwyn Mathew SamAwardedAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Mr Christopher Britton ReynoldsL3HarrisAwardedAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Mitchell L PassarelliGeorgia Institute of TechnologyAwardedAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Dr WingFai NgTechsburg, Inc.AwardedAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwardAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Dan M GoebelJet Propulsion Laboratory (JPL)AwardedAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Mrs Sarah W SharkAerojet RocketdyneAwardedAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Dr Trevor S ElliottUniversity of Tennessee at ChattanoogaAwardedAward: “Comparative Analysis and Justification of Optimal Rocket Motor Selection in NASA USLI by Applying Newton’s Second Law to a Variable Mass Body” (AIAA 2019-4138)
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Mr Vedant Kiritkumar MehtaAwardedAward: 2019 AIAA Aerospace Power Systems Best Student Paper Competition AwardAIAA Citation: “Hydrogen Loss Effects on Mircoreactors for Space and Planetary Nuclear Power Production” (AIAA 2019-4452)
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Dr Richard R HoferJet Propulsion Laboratory (JPL)AwardedAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Dr Scott J HallOrbion Space TechnologyAwardedAward: 2019 AIAA Electric Propulsion Best Paper AwardAIAA Citation: “High Power Demonstration of a 100 kW Nested Hall Thruster System (AIAA-2019-3809)
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Dr Krishna VenkatesanGE AerospaceAwardedAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Arin E. L. CrossGE AerospaceAwardedAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Dr Jonathan L FlemingTechsburgAwardedAward: 2019 AIAA Inlets, Nozzles, and Propulsion System Integration Best Paper AwardAIAA Citation: “Development of a Ducted Propulsor for BLI Electric Regional Aircraft – Part I: Aerodynamic Design and Analysis” (AIAA-2019-3853)
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Dr Robert A BaurleAir Force Research LaboratoryAwardedAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Dr Fabian ChaconGeneral Electric / InnoveeringAwardedAward: Study of Parasitic Combustion in an Optically Accessible Continuous Wave Rotating Detonation Engine (AIAA 2019-0473)AIAA Citation: 2019 AIAA High Speed Air Breathing Propulsion Best Paper
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Dr Jeffrey P BonsOhio State UniversityAwardedAward: 2020 AIAA Gas Turbine Engines Best Paper AwardAIAA Citation: “Conjugate Heat Transfer Study of Innovative Pin-Fin Cooling Configuration ” (AIAA-2020-0634)
-
Alessandro RuffinAwardedAward: the 2019 AIAA Hybrid Rockets Best Paper AwardAIAA Citation: “Real Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor” (AIAA 2019-4266)
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ENS David L EllisNASA Glenn Research CenterAwardedAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
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Dr Paul M DanehyNASA Langley Research CenterAwardedAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Eric PittmanAwardedAward: 2019 AIAA Propulsion Education Best Student Paper AwardAIAA Citation: “Development and Experimentation of a Lab-Scale Pulse Detonation Engine (PDE)” (AIAA 2019-3808)
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Dr Timothy M WabelThe Aerospace CorporationAwardedAward: the 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Prof Adam M SteinbergGeorgia Institute of TechnologyAwardedAward: 2019 AIAA Propellants and Combustion Best Paper AwardAIAA Citation: “Influence of Cross-Frequency Interactions on Nonstationary Thermoacoustic Oscillations in a Rich-Burn Gas Turbine Combustor at Elevated Pressure” (AIAA-2019-3949)
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Daniel J LevackL3HarrisAwardedAward: 2019 AIAA Nuclear and Future Flight Best Paper AwardAIAA Citation: “Applications of Nuclear Thermal Propulsion to Lunar Architectures” (AIAA 2019-4032)
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Dr Brian J CantwellStanford UniversityAwardedAward: 2019 AIAA Hybrid Rockets Best Student Paper AwardAIAA Citation: “Experimental Findings on Pre- and Post-combustion Chamber Effects in a Laboratory-scale motor” (AIAA 2019-4336)
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Robin HuntNASA Langley Research CenterAwardedAward: 2019 AIAA High Speed Air Breathing Propulsion Best Paper AwardAIAA Citation: “Using Computational Flow Imaging to Optimize Filtered Rayleigh Scattering Measurements of an Isolator Shock Train” (AIAA 2019-4016)
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Chance P GarciaAwardedAward: 2019 ASME Aerospace Division Propulsion Technical Committee Best Paper AwardAIAA Citation: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-Cooled Combustion Chambers” (AIAA 2019-4228)
2019
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Dr Noel T ClemensThe University of Texas at AustinAwardedAward: 2019 HSABP Best PaperAIAA Citation: “Supersonic Isolator Shock-Train Dynamics: Simple Physics-Based Model for Closed Loop Control of Shock Train Location” (AIAA 2018-1618
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Dr Leon VanstoneHyperSciencesAwardedAward: 2019 HSABP Best PaperAIAA Citation: “Supersonic Isolator Shock-Train Dynamics: Simple Physics-Based Model for Closed Loop Control of Shock Train Location” (AIAA 2018-1618
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Dr Vlad J HrubyBusek Co, Inc.AwardedAward: 2018 Electric Propulsion Best PaperAIAA Citation: “In-Flight Verification and Validation of Colloid Microthruster Performance” (AIAA 2018-4643)
2018
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Mr David WoernerJet Propulsion LaboratoryAwardedAward: 2017 Aerospace Power Systems Best PaperAIAA Citation: Next-Generation RTGs for NASA (AIAA 2017-4612)
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Dr John C Melcher IVNASA-Johnson Space CenterAwardedAward: 2017 Liquid Propulsion Best PaperAIAA Citation: Coil-On-Plug Ignition for Oxygen/Methane Liquid Rocket Engines in Thermal-Vacuum Environments (AIAA 2017-4666)
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Dr Tristan A HearnNASA Glenn Research CenterAwardedAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Stefanie M HirtNASA Glenn Research CenterAwardedAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Mr Dillon P SlussAwardedAward: 2017 Solid Rockets Best PaperAIAA Citation: “Biglobal Stability of the Swirling Majdalani-Fist Mean Flowfield in Solid Rocket Motors” (AIAA 2017-4949)
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Mr Wesley A Gibson
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William CooganFirefly AerospaceAwardedAward: 2017 Electric Propulsion Best PaperAIAA Citation: “A Critical Review of Thrust Models for Applied-Field Magnetoplasmadynamic Thrusters” (AIAA 2017-4723),
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Mr. David J ArendNASA Glenn Research CenterAwardedAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Dr Carmine CarmicinoUniversità di Napoli Federico IIAwardedAward: 2018 Hybrid Rockets Best PaperAIAA Citation: An Analytical Model to Predict Longitudinal Acoustic Modes Frequency of Hybrid Rockets Combustion Chamber (AIAA 2017-4645)
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Dr Larry W HardinRTXAwardedAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Dr Trevor S ElliottUniversity of Tennessee at ChattanoogaAwardedAward: 2017 Solid Rockets Best PaperAIAA Citation: “Biglobal Stability of the Swirling Majdalani-Fist Mean Flowfield in Solid Rocket Motors” (AIAA 2017-4949)
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Prof Dario PastronePolitecnico di TorinoAwardedAward: 2018 Hybrid Rockets Best PaperAIAA Citation: An Analytical Model to Predict Longitudinal Acoustic Modes Frequency of Hybrid Rockets Combustion Chamber (AIAA 2017-4645)
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Mr John D WolterNASA Glenn Research CenterAwardedAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
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Prof Edgar ChoueiriPrinceton UniversityAwardedAward: 2017 Electric Propulsion Best PaperAIAA Citation: [email protected]
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John A GazzanigaHx5, LLCAwardedAward: 2018 Inlets, Nozzles, and Propulsion Systems Integration Best PaperAIAA Citation: “Performance Calculations for a Boundary-Layer-Ingesting Fan Stage from Sparse Measurements” (AIAA 2018-1889)
2017
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Mr Michael L EverettUniversity of Texas at El PasoAwardedAward: K-12 Minority STEM Education Program: MAA SouthwestAIAA Citation: K-12 Minority STEM Education Program: MAA Southwest
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Prof Claude Russell Joyner IIL3HarrisAwardedAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Mr. Francois ChedevergneENSAE SupaeroAwardedAward: Local Linear Stability Analysis of Non-Circular Injection-Driven Channel FlowsAIAA Citation: AIAA 2016-4701
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Dr Luciano GalfettiPolitecnico di MilanoAwardedAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Mr Jakub GlowackiAwardedAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Mr Manabu TanakaAwardedAward: Fundamental Studies of Radio-Frequency Preionization for Frozen Inert Gas Plasma Magnetohydrodynamic Electric Power GenerationAIAA Citation: Fundamental Studies of Radio-Frequency Preionization for Frozen Inert Gas Plasma Magnetohydrodynamic Electric Power Generation
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Richard W WarwickLockheed Martin Space SystemsAwardedAward: Solar Array Design for the Mars InSight Lander Mission,”AIAA Citation: Solar Array Design for the Mars InSight Lander Mission,”
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Mr Maxime BouygesONERAAwardedAward: Local Linear Stability Analysis of Non-Circular Injection-Driven Channel FlowsAIAA Citation: AIAA 2016-4701
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Dr Chana GoldbergN/AAwardedAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Joseph CarneyAwardedAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Dr Samantha J. AlbertsThe Boeing CompanyAwardedAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Mr Jasper GrohmannGerman Aerospace Center (DLR)AwardedAward: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustorAIAA Citation: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustor
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Mr Michael EadesMichael EadesAwardedAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Dr Steven B StanleyBlue Origin LLCAwardedAward: Experimental Investigation of Continuous Detonation Rocket Engines for In-Space Propulsion”AIAA Citation: Experimental Investigation of Continuous Detonation Rocket Engines for In-Space Propulsion”
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Dr Paolo VenneriUSNCAwardedAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Dr Devaiah K NaliandaAwardedAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Mr Aaron W SkibaAwardedAward: Experimental Assessment of Premixed Flames Subjected to Extreme TurbulenceAIAA Citation: Experimental Assessment of Premixed Flames Subjected to Extreme Turbulence
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Scott A. BilletsAwardedAward: Solar Array Design for the Mars InSight Lander Mission,”AIAA Citation: Solar Array Design for the Mars InSight Lander Mission,”
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Dr Timothy OmbrelloAir Force Research LaboratoryAwardedAward: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”AIAA Citation: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”
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Dr Christian ParavanPolitecnico di MilanoAwardedAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Prof James F DriscollUniversity of MichiganAwardedAward: Experimental Assessment of Premixed Flames Subjected to Extreme TurbulenceAIAA Citation: Experimental Assessment of Premixed Flames Subjected to Extreme Turbulence
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Stefania CarlottiAwardedAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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John R AndersonJet Propulsion LaboratoryAwardedAward: Mechanics for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanics for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Mr Bastian RauchAwardedAward: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustorAIAA Citation: Investigation of differences in lean blowout of liquid single-component fuels in a gas turbine model combustor
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Prof Benjamin JornsUniversity of Michigan, Ann ArborAwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Filippo MaggiPolitecnico Di MilanoAwardedAward: Vortex Combustion in a Lab-Scale Hybrid Rocket MotorAIAA Citation: AIAA 2016-4562
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Mr Praveen SrikanthConvergent ScienceAwardedAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Prof Gregoire CasalisONERAAwardedAward: Local Linear Stability Analysis of Non-Circular Injection-Driven Channel FlowsAIAA Citation: AIAA 2016-4701
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Dr Leslie A SmithSierra Nevada CorporationAwardedAward: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”AIAA Citation: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”
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Dr Norman D Love JrThe University of Texas El PasoAwardedAward: K-12 Minority STEM Education Program: MAA SouthwestAIAA Citation: K-12 Minority STEM Education Program: MAA Southwest
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Dr Dan M GoebelJet Propulsion Laboratory (JPL)AwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Luke B RobersonNASA-Kenndey Space CenterAwardedAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Dr Richard R HoferJet Propulsion Laboratory (JPL)AwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Jacob TemmeU. S. Army Research Laboratory (APG)AwardedAward: Experimental Assessment of Premixed Flames Subjected to Extreme TurbulenceAIAA Citation: Experimental Assessment of Premixed Flames Subjected to Extreme Turbulence
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Mr Giang Q LamLockheed Martin Space SystemsAwardedAward: Solar Array Design for the Mars InSight Lander MissionAIAA Citation: Solar Array Design for the Mars InSight Lander Mission
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Christopher A DodsonRelativity SpaceAwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Enrico CavalliniAgenzia Spaziale ItalianaAwardedAward: Motor Scale and Propellant Geometry Effects on Pressure Oscillations in Aft-Finocyl Solid Rocket MotorsAIAA Citation: AIAA 2016-4793
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Dr David G MacManusCranfield UniversityAwardedAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Mr Charles J Moore JrNASA Kennedy Space CenterAwardedAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Prof Adam P BrucknerAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Mr Sebastian OkhovatBellAwardedAward: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”AIAA Citation: AIAA 2017-1538, “ The Effect of Pulsed Injection on the Entrainment into a Cavity Based Flameholder in Supersonic Flow,”
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Dr Alejandro Lopez OrtegaJet Propulsion Laboratory (JPL)AwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Dr Michael J SekerakJohns Hopkins University Applied Physics LaboratoryAwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Mr Vishal PatelUltra Safe Nuclear CorporationAwardedAward: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion SystemsAIAA Citation: Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems
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Prof Steven H CollicottPurdue UniversityAwardedAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Mr. John D GlassAnalex Corporation HeadquartersAwardedAward: “Thermal-Mechanical Characterization of Bridgewires and Surrounding Materials Utilizing Thermal Transient Testing”AIAA Citation: AIAA 2016-4932
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Dr Stephen D HeisterPurdue UniversityAwardedAward: Experiment Design for Measuring Accommodation Coefficients for Modeling of Long-Duration Spaceflight Cryogenic PropellantsAIAA Citation: AIAA 2015-4246
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Pericles PilidisCranfield UniversityAwardedAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Dr Ahsan R ChoudhuriUniversity of Texas at El PasoAwardedAward: K-12 Minority STEM Education Program: MAA SouthwestAIAA Citation: K-12 Minority STEM Education Program: MAA Southwest
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Jeffrey F GlusmanAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Richard D GristAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Mr James L FelderNASA Glenn Research CenterAwardedAward: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design PointAIAA Citation: Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point
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Dr Ioannis G MikellidesJet Propulsion Laboratory (JPL)AwardedAward: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall ThrusterAIAA Citation: Mechanisms for Pole Piece Erosion in a 6-kW Magnetically-Shielded Hall Thruster
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Prof Andrew J HigginsMcGill UniversityAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Prof Carl KnowlenUniversity of WashingtonAwardedAward: Experimental Investigation of a Baffled-Tube Ram AcceleratorAIAA Citation: Experimental Investigation of a Baffled-Tube Ram Accelerator
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Dr Agostino NeriEuropean Space Agency (ESA)AwardedAward: Motor Scale and Propellant Geometry Effects on Pressure Oscillations in Aft-Finocyl Solid Rocket MotorsAIAA Citation: AIAA 2016-4793
2016
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Prof Claude Russell Joyner IIL3HarrisAwardedAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Dr Stanley K Borowskiretired, NASA Glenn Research CenterAwardedAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Michael BeyarBoeing Research & TechnologyAwardedAward: Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Mr David R McCurdyVantage Partners, LimitedAwardedAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Prof Grant A RishaPennsylvania State University AltoonaAwardedAward: Multi-Injector Impinging Jet Studies of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic ParticlesAIAA Citation: AIAA 2015-3972
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Jeff D FlammNASA Langley Research CenterAwardedAward: Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Dr Kurtis R LongArc-Aox, Experimental Aerophyscis BranchAwardedAward: Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Dr Christopher C DanielsAwardedAward: Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Philip IvancicAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr Luciene D VillarInstitute of Aeronautics and SpaceAwardedAward: Time-Temperature Superposition Principle Applied to Thermally Aged Composite PropellantAIAA Citation: AIAA 2015-4107
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Dr Kohei OzawaKyushu Institute of TechnologyAwardedAward: “Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors”AIAA Citation: AIAA 2015-3832
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Dr David LiuSecretary of the Air Force - Global Power DirectorateAwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr Campbell D CarterU.S. Air Force Research LaboratoryAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr Ez A HassanAir Force Research LaboratoryAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Prof Benveniste NatanTechnion - Israel Institute of TechnologyAwardedAward: Multi-Injector Impinging Jet Studies of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic ParticlesAIAA Citation: AIAA 2015-3972
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Mr. Rafael A MartinezAwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr Timothy OmbrelloAir Force Research LaboratoryAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Ms Luisa A Cabrera MaynezAwardedAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Dr Arne SeitzGerman Aerospace Center DLR e.V.AwardedAward: A Composite Cycle Engine Concept with Hecto-Pressure RatioAIAA Citation: AIAA 2015-4028
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Dr David M PetersonAir Force Research LaboratoryAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Dr John D WilliamsColorado State UniversityAwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Daniel M TompkinsBoeing Research and TechnologyAwardedAward: Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Dr Minel BraunThe University of AkronAwardedAward: Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Mr Terrence L Connell JrThe Pennsylvania State UniversityAwardedAward: Multi-Injector Impinging Jet Studies of Ignition Delay for Hydrogen Peroxide and Gelled Hydrocarbon Fuel Containing Reactive or Catalytic ParticlesAIAA Citation: AIAA 2015-3972
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Dr Keith A GonthierLouisiana State UniversityAwardedAward: “Analysis of Dissipation Induced by Successive Planar Shock Loading of Granular Explosive”AIAA Citation: AIAA 2015-3708
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Mr Manuel J HernandezAwardedAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Mr Greg ZilliacNASA Ames Research CenterAwardedAward: “Visualization Study of Self-Pressurizing Propellant Tank Dynamics”AIAA Citation: AIAA 2015-3829
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Dr Norman D Love JrThe University of Texas El PasoAwardedAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Mr. James E WernerIdaho National LaboratoryAwardedAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015=3774
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Dr Arthur Louis QuallsOak Ridge National LaboratoryAwardedAward: Affordable Development and Demonstration of a Small NTR Engine and Stage: A Preliminary NASA, DOE and Industry AssessmentAIAA Citation: AIAA 2015-3774
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Kevin D JamesNASA-Ames Research CenterAwardedAward: Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Carl R MullinsBusek Co. Inc.AwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Edward A LukeMississippi State UniversityAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Prof Hyungrok DoSeoul National UniversityAwardedAward: “Establishing the Controlling Parameters of Ignition in High-Speed Flow”AIAA Citation: AIAA 2016-0658
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Pratap Thamanna RaoLouisiana State UniversityAwardedAward: “Analysis of Dissipation Induced by Successive Planar Shock Loading of Granular Explosive”AIAA Citation: AIAA 2015-3708
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Andrew S FistAwardedAward: Improved Mean Flow Solution for Solid Rocket Motors with a Naturally Developing Swirling MotionAIAA Citation: AIAA 2014-4016
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Dr Toru ShimadaJapan Aerospace Exploration AgencyAwardedAward: “Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors”AIAA Citation: AIAA 2015-3832
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Dr Olga V KartuzovaCase Western Reserve UniversityAwardedAward: CFD Modeling of the Multipurpose Hydrogen Test Bed (MHTB) Self-Pressurization and Spray Bar Mixing Experiments in Normal Gravity: Effect of the Accommodation Coefficient on the Tank PressureAIAA Citation: AIAA 2015-3769
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Prof Joseph MajdalaniAuburn UniversityAwardedAward: Improved Mean Flow Solution for Solid Rocket Motors with a Naturally Developing Swirling MotionAIAA Citation: AIAA 2014-4016
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Dr Casey C FarnellColorado State UniversityAwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Mr Sascha KaiserBauhaus Luftfahrt e. V.AwardedAward: A Composite Cycle Engine Concept with Hecto-Pressure RatioAIAA Citation: AIAA 2015-4028
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Dr Mohammad KassemiNASA Glenn Research CenterAwardedAward: CFD Modeling of the Multipurpose Hydrogen Test Bed (MHTB) Self-Pressurization and Spray Bar Mixing Experiments in Normal Gravity: Effect of the Accommodation Coefficient on the Tank PressureAIAA Citation: AIAA 2015-3769
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Dr Ahsan R ChoudhuriUniversity of Texas at El PasoAwardedAward: Component and System Modeling of a Direct Power Extraction SystemAIAA Citation: AIAA 2016-0990
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Shawn C TaylorNASA Glenn Research CenterAwardedAward: Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Dr Heather Ann OravecThe University of AkronAwardedAward: Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
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Mr Jonah E ZimmermanAwardedAward: “Visualization Study of Self-Pressurizing Propellant Tank Dynamics”AIAA Citation: AIAA 2015-3829
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Dr Brian J CantwellStanford UniversityAwardedAward: “Visualization Study of Self-Pressurizing Propellant Tank Dynamics”AIAA Citation: AIAA 2015-3829
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Dr Patrick R SheaNASA Langley Research CenterAwardedAward: Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration”AIAA Citation: AIAA 2016-0011
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Mr. Cody C FarnellColorado State UniversityAwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Dr Richard D BranamUS Air Force Academy, HQ USAFA/DFANAwardedAward: “Non-Invasive Hall Current Distribution Measurement in a Hall Effect Thruster”AIAA Citation: AIAA 2015-4005
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Janice WasowskiAwardedAward: Leak Rate Quantification Method for Gas Pressure Seals with Controlled Pressure Differential”AIAA Citation: AIAA 2015-4231
2015
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Dr Martin ReinDLR - German Aerospace CenterAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Eur Ing Luis P Ruiz-CalaveraAIRBUS Defence and SpaceAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Dr Thomas M BerensAIRBUS Defence and SpaceAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mrs Anne-Laure DELOTONERAAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mr. Michael SaterskogHjortronvagen 73AwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Dr Nicola CeresolaAlenia AeronauticaAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mr David E Funes-SebastianAIRBUS Defence and SpaceAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
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Mr Magnus H TormalmFOIAwardedAward: “Numerical and Experimental Investigations on Highly Integrated Subsonic Air Intakes”AIAA Citation: AIAA 2014-0722
2014
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Dr Stanley K Borowskiretired, NASA Glenn Research CenterAwardedAward: A One-year Round Trip Crewed Mission to Mars using Bimodal Nuclear Thermal and Electric Propulsion (BNTEP)AIAA Citation: AIAA 2013-4076
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Vincent Caux-BriseboisAwardedAward: Thermo-Acoustic Coupling in Swirl-Stabilized Flames with Helical VorticesAIAA Citation: AIAA 2013-3650
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Dr James E PolkJet Propulsion Laboratory (JPL)AwardedAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
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Mr David R McCurdyVantage Partners, LimitedAwardedAward: A One-year Round Trip Crewed Mission to Mars using Bimodal Nuclear Thermal and Electric Propulsion (BNTEP)AIAA Citation: AIAA 2013-4076
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Mr Jeffrey CsankNASA Glenn Research CenterAwardedAward: 2013 ASME Best Propulsion PaperAIAA Citation: Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter Approach (AIAA 2013-4002)
-
Michael McPhersonDigital Solid State PropulsionAwardedAward: Electric Solid Propellants: A Safe, Micro to Macro Propulsion TechnologyAIAA Citation: AIAA 2013-4168
-
Dr Benjamin S WaxmanNoneAwardedAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
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Dr Daniele PavarinUniversità degli Studi di PadovaAwardedAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
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Dr Alberto BettellaCISAS-University of PadovaAwardedAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
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Ms. Laura M BurkeNASA-Glenn Research CenterAwardedAward: A One-year Round Trip Crewed Mission to Mars using Bimodal Nuclear Thermal and Electric Propulsion (BNTEP),”AIAA Citation: AIAA 2013-4076
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Dr Wayne N SawkaDSSP INCAwardedAward: Electric Solid Propellants: A Safe, Micro to Macro Propulsion TechnologyAIAA Citation: AIAA 2013-4168
-
Mr Greg ZilliacNASA Ames Research CenterAwardedAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
-
Dr Dan M GoebelJet Propulsion Laboratory (JPL)AwardedAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
-
Dr Hans-Detlev KuehlTU Dortmund UniversityAwardedAward: A Review of Models for Appendix Gap Losses in Stirling Cycle MachinesAIAA Citation: AIAA 2013-3613
-
Mrs Amy K ChicatelliHX5, LLCAwardedAward: Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter ApproachAIAA Citation: AIAA 2013-4002
-
Dr Richard R HoferJet Propulsion Laboratory (JPL)AwardedAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
-
Dr Ira KatzJet Propulsion LaboratoryAwardedAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
-
Dr Robert John YentschAwardedAward: Unsteady Three-Dimensional Phenomena in Mode-Transition Simulations of the HIFiRE-2 Scramjet FlowpathAIAA Citation: AIAA 2013-3753
-
Mr Jens PfeifferLaboratory of ThermodynamicsAwardedAward: A Review of Models for Appendix Gap Losses in Stirling Cycle MachinesAIAA Citation: AIAA 2013-3613
-
Prof Hyoung Jin KimKyung Hee UniversityAwardedAward: Optimal Inlet Shape Design of N2B Hybrid Wing Body ConfigurationAIAA Citation: AIAA 2012-3917
-
Dr Philipp BehruziArianeGroupAwardedAward: Passive Phase Separation in Cryogenic Upper Stage TanksAIAA Citation: AIAA 2013-3905
-
Mr Christoph Michael ArndtGerman Aerospace Center (DLR)AwardedAward: Thermo-Acoustic Coupling in Swirl-Stabilized Flames with Helical VorticesAIAA Citation: AIAA 2013-3650
-
Joseph W ConnollyNASA Glenn Research CenterAwardedAward: Model-Based Control of a Nonlinear Aircraft Engine Simulation using an Optimal Tuner Kalman Filter ApproachAIAA Citation: AIAA 2013-4002
-
Dr Datta V GaitondeThe Ohio State UniversityAwardedAward: Unsteady Three-Dimensional Phenomena in Mode-Transition Simulations of the HIFiRE-2 Scramjet FlowpathAIAA Citation: AIAA 2013-3753
-
Eur Ing Federico MorettoUniversita di PadovaAwardedAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
-
Prof Adam M SteinbergGeorgia Institute of TechnologyAwardedAward: Thermo-Acoustic Coupling in Swirl-Stabilized Flames with Helical VorticesAIAA Citation: AIAA 2013-3650
-
Mr Jonah E ZimmermanAwardedAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
-
Dr Brian J CantwellStanford UniversityAwardedAward: Mass Flow Rate and Isolation Characteristics of Injectors for Use with Self-Pressurizing Oxidizers in Hybrid RocketsAIAA Citation: AIAA 2013-3636
-
Mr Nicolas BellomoAwardedAward: Development and Flight Testing of a Hybrid Rocket Booster for UAV Assisted Take OffAIAA Citation: AIAA 2013-4140
-
Salvatore M OritiNASA Glenn Research CenterAwardedAward: Performance Measurement of Advanced Stirling Convertors (ASC-E3)AIAA Citation: AIAA 2013-3813
-
Dr Ioannis G MikellidesJet Propulsion Laboratory (JPL)AwardedAward: Conducting Wall Hall ThrustersAIAA Citation: AIAA 2013-4117
2013
-
Mr. Andrew J SlippeyRochester Institute of TechnologyAwardedAward: “Long-Lived Venus Lander Thermal Management System Design”AIAA Citation: AIAA 2012-3892
-
William S BlackAwardedAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion SystemsAIAA Citation: AIAA 2013-4263
-
Shannon D EilersAwardedAward: “Development and Testing of the Regeneratively Cooled Multiple Use Plug Hybrid (for) Nanosats (MUPHyN) Motor”AIAA Citation: AIAA 2013-4199
-
Dr Travis C FisherSandia National LaboratoriesAwardedAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion SystemsAIAA Citation: AIAA 2013-4263
-
Miss Rebecca Lynn HayAdvanced Cooling Technologies, IncAwardedAward: “Long-Lived Venus Lander Thermal Management System Design”AIAA Citation: AIAA 2012-3892
-
Dr Jean-luc EstivalezesONERAAwardedAward: Theoretical Investigation of Parietal Vortex Shedding in Solid Rocket MotorsAIAA Citation: AIAA 2012-3825
-
Jeffery A WhiteNASA-Langley Research CenterAwardedAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion SystemsAIAA Citation: AIAA 2012-4263
-
Prof Christian O PaschereitTechnische Universität BerlinAwardedAward: “Influence of Steam Dilution on NOx Formation in Premixed Natural Gas and Hydrogen Flames,”AIAA Citation: AIAA 2012-1272
-
Jan DeekenDLR-German Aerospace CenterAwardedAward: Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation ConditionsAIAA Citation: AIAA 2012-3867
-
Mr Pete F CrudgingtonCross Manufacturing Company (1938) LtdAwardedAward: , “A Novel High temperature non-Contact Dynamic Seal”AIAA Citation: AIAA 2012-4004
-
Prof Nicholas SyredCardiff UniversityAwardedAward: Tangential Velocity Effects and Correlations for Blow-Off and Flashback in a Generic Swirl Burner and the Effect of a Hydrogen containing FuelAIAA Citation: AIAA 2013-0736
-
Dr Dimitry SuslovDLR - German Aerospace CenterAwardedAward: Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation ConditionsAIAA Citation: AIAA 2012-3867
-
Dr Jesse QuinlanNASA Aeronautics Research Mission DirectorateAwardedAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion SystemsAIAA Citation: AIAA 203-4263
-
Dr Stephen A WhitmoreUtah State UniversityAwardedAward: “Development and Testing of the Regeneratively Cooled Multiple Use Plug Hybrid (for) Nanosats (MUPHyN) Motor”AIAA Citation: AIAA 2013-4199
-
Ms Kimberly SaviersAwardedAward: Carbon Nanotube Arrays for Enhanced Thermal Interfaces to Thermoelectric ModulesAIAA Citation: AIAA 2012-4048
-
Prof Gregoire CasalisONERAAwardedAward: Theoretical Investigation of Parietal Vortex Shedding in Solid Rocket MotorsAIAA Citation: AIAA 2012-3825
-
Dr Dan M GoebelJet Propulsion Laboratory (JPL)AwardedAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with ExperimentAIAA Citation: AIAA 2012-3789
-
Prof Timothy S FisherUCLAAwardedAward: Carbon Nanotube Arrays for Enhanced Thermal Interfaces to Thermoelectric ModulesAIAA Citation: AIAA 2012-4048
-
Dr Richard R HoferJet Propulsion Laboratory (JPL)AwardedAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with ExperimentAIAA Citation: AIAA 2012-3789
-
Mr Zachary W PetersonAwardedAward: “Development and Testing of the Regeneratively Cooled Multiple Use Plug Hybrid (for) Nanosats (MUPHyN) Motor”AIAA Citation: AIAA 2013-4199
-
Dr Ira KatzJet Propulsion LaboratoryAwardedAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with ExperimentAIAA Citation: AIAA 2012-3789
-
Prof Oskar J HaidnTechnische Universität MünchenAwardedAward: Investigation of the API-Injection Concept in a LOX/LH2 Combustion Chamber at GG/PB Operation ConditionsAIAA Citation: AIAA 2012-3867
-
Mr Germain BoyerAwardedAward: Theoretical Investigation of Parietal Vortex Shedding in Solid Rocket MotorsAIAA Citation: AIAA 2012-3825
-
Dr Meng-Sing LiouNASA Glenn Research CenterAwardedAward: Optimal Inlet Shape Design of N2B Hybrid Wing Body ConfigurationAIAA Citation: AIAA 2013-3917
-
Dr P. J. BowenCardiff UniversityAwardedAward: Tangential Velocity Effects and Correlations for Blow-Off and Flashback in a Generic Swirl Burner and the Effect of a Hydrogen containing FuelAIAA Citation: AIAA 2013-0736
-
Dr Robert A BaurleAir Force Research LaboratoryAwardedAward: “Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion SystemsAIAA Citation: AIAA 2012-4263
-
ENS Eric W DavisThe Aerospace CorporationAwardedAward: Faster-Than-Light Space Warps, Status and Next StepsAIAA Citation: AIAA 2012-3860
-
Dr Calin TarauAdvanced Cooling TechnologiesAwardedAward: “Long-Lived Venus Lander Thermal Management System Design”AIAA Citation: AIAA 2012-3892
-
Dr Ioannis G MikellidesJet Propulsion Laboratory (JPL)AwardedAward: “Design of a Laboratory Hall Thruster with Magnetically Shielded Channel Walls, Phase III: Comparison of Theory with ExperimentAIAA Citation: AIAA 2012-3789
2012
-
Dr Stanley K Borowskiretired, NASA Glenn Research CenterAwardedAward: “Lower Thrust Engine Options Based on the Small Nuclear Rocket Engine Design”AIAA Citation: AIAA 2011-5846
-
Kazutoshi IshikawaNational Aerospace LaboratoriesAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Eur Ing Francesco Baratouniversità degli studi di PadovaAwardedAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
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Dr Luciano GalfettiPolitecnico di MilanoAwardedAward: “Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion”AIAA Citation: AIAA 2011-5680
-
Charles E GarnerJet Propulsion LaboratoryAwardedAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
-
Prof Fletcher J. MillerSan Diego State UniversityAwardedAward: Design and Analysis of a Multi-Window Aperture Structure for a Small Particle Solar ReceiverAIAA Citation: AIAA 2011-5900
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Eur Ing Marta LazzarinCISAS-University of PadovaAwardedAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
-
Dr Martina FaenzaNammo Raufoss ASAwardedAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
-
Prof M. MungalStanford UniversityAwardedAward: “Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow”AIAA Citation: AIAA 2011-0319
-
Dr Mirko GambaUniversity of MichiganAwardedAward: “Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow”AIAA Citation: AIAA 2011-3539
-
Dr Luigi De LucaPolitecnico Di MilanoAwardedAward: “Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion”AIAA Citation: AIAA 2011-5680
-
Dr Yutaka UmemuraJAXAAwardedAward: Heat Exchange and Pressure Drop Enhanced by SloshingAIAA Citation: AIAA 2011-5682
-
Mr Daizo SugimoriJapan Aerospace Exploration AgencyAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Dr Satoshi NonakaJapan Aerospace Exploration AgencyAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Dr Campbell D CarterU.S. Air Force Research LaboratoryAwardedAward: “Particle Image Velocimetry in an Isothermal and Exothermic High-Speed Cavity”AIAA Citation: AIAA 2012-0330
-
A. Scott HoweJet Propulsion LaboratoryAwardedAward: “Habitat Water Wall for Water, Solids, and Atmosphere Recycle and Reuse”AIAA Citation: AIAA 2011-5018
-
Dr KuangYu HsuInnovative Scientific Solutions IncorporatedAwardedAward: “Particle Image Velocimetry in an Isothermal and Exothermic High-Speed Cavity”AIAA Citation: AIAA 2012-0330
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Dr Daniele PavarinUniversità degli Studi di PadovaAwardedAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
-
Dr Alberto BettellaCISAS-University of PadovaAwardedAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
-
Mr Nathan GibsonGE Aerospace ResearchAwardedAward: Second Generation Air-to-Air Mechanical Seal Design and PerformanceAIAA Citation: AIAA 2011-5636
-
Prof Chihiro InoueUniversity of TokyoAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Dr Filippo MaggiPolitecnico Di MilanoAwardedAward: “Ballistic and Rheological Characterization of Paraffin-Based Fuels for Hybrid Rocket Propulsion”AIAA Citation: AIAA 2011-5680
-
Mr James E FittjeSAICAwardedAward: “Lower Thrust Engine Options Based on the Small Nuclear Rocket Engine Design”AIAA Citation: AIAA 2011-5846
-
Maxwell H BriggsAwardedAward: 2011 Aerospace Power Systems Best PaperAIAA Citation: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling Convertor (AIAA 2011-5576)
-
Mr. Steven MikesJet Propulsion LaboratoryAwardedAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
-
Dr Mark SalitaAwardedAward: Unanticipated Problems and Misunderstood Phenomena in and Around Solid RocketsAIAA Citation: AIAA 2011-5956
-
Dr Kohei OkitaThe University of TokyoAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Ioana Diana BroomeAwardedAward: Design and Analysis of a Multi-Window Aperture Structure for a Small Particle Solar ReceiverAIAA Citation: AIAA 2011-5900
-
Bruce G SchnitzlerOak Ridge National LabAwardedAward: “Lower Thrust Engine Options Based on the Small Nuclear Rocket Engine Design”AIAA Citation: AIAA 2011-5846
-
Yoshihiro NaruoJapan Aerospace Exploration AgencyAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Dr Terry V Reid SrNASA Glenn Research CenterAwardedAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
-
Daniel N MillerLockheed Martin AeronauticsAwardedAward: “Addressing Corner Interactions Generated by Oblique Shock-Waves In Unswept Right-Angle Corners and Implications for High-Speed Inlets”AIAA Citation: AIAA 2012-0275
-
Dr Yoshifumi InataniJapan Aerospace Exploration AgencyAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Dr Steven G TuttleNaval Surface Warfare Center, Indian HeadAwardedAward: “Particle Image Velocimetry in an Isothermal and Exothermic High-Speed Cavity”AIAA Citation: AIAA 2012-0330
-
Prof Takehiro HimenoUniversity of TokyoAwardedAward: Heat Exchange and Pressure Drop Enhanced by SloshingAIAA Citation: AIAA 2011-5682
-
Dan BaruzziniRolls-Royce CorpAwardedAward: “Addressing Corner Interactions Generated by Oblique Shock-Waves In Unswept Right-Angle Corners and Implications for High-Speed Inlets”AIAA Citation: AIAA 2012-0275
-
Dr Malak F MalakAllied Signal Aerospace CoAwardedAward: Second Generation Air-to-Air Mechanical Seal Design and PerformanceAIAA Citation: AIAA 2011-5636
-
Nicholas A SchiferNASAAwardedAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
-
John R BrophyJet Propulsion Laboratory (JPL)AwardedAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
-
Dr Marc D RaymanNASA/JPLAwardedAward: In-Flight Operation of the Dawn Ion Propulsion System Through Orbit Capture at VestaAIAA Citation: AIAA 2011-5661
-
Prof Toshinori WatanabeThe University of TokyoAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Prof Kiyoshi KinefuchiNagoya UniversityAwardedAward: “Heat Exchange and Pressure Drop Enhanced by Sloshing”AIAA Citation: AIAA 2011-5682
-
Scott D WilsonNASA Glenn Research CenterAwardedAward: Overview of Heat Addition and Efficiency Predictions for an Advanced Stirling ConvertorAIAA Citation: AIAA 2011-5576
-
Prof Ronald K HansonStanford UniversityAwardedAward: “Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow”AIAA Citation: AIAA 2011-0319
-
Prof Ashwani K GuptaUniversity of MarylandAwardedAward: “Mixture Preparation Effects On Distributed Combustion For Gas Turbine Applications”AIAA Citation: AIAA 2012-0930
-
Mr Nicolas BellomoAwardedAward: “A Numerical Model to Analyze the Transient Behavior and Instabilities on Hybrid Rocket Motors”AIAA Citation: AIAA 2011-5538
-
Dr Neal D DomelLockheed Martin AeronauticsAwardedAward: Addressing Corner Interactions Generated by Oblique Shock-Waves In Unswept Right-Angle Corners and Implications for High-Speed InletsAIAA Citation: IAA 2012-0275
2011
-
Mr John T LopezAwardedAward: Quantifying the Effects of Long Term Storage on Extended Cycling for Lithium-Ion BatteriesAIAA Citation: AIAA 2010-6924
-
CPT Paul M HradAwardedAward: Conceptual Design Tool for Micro Air Vehicles with Hybrid Power SystemsAIAA Citation: AIAA 2010-6688
-
Dr Frederick G HarmonAFITAwardedAward: Conceptual Design Tool for Micro Air Vehicles with Hybrid Power SystemsAIAA Citation: AIAA 2010-6688
-
Mr. Chris D PearsonAwardedAward: Quantifying the Effects of Long Term Storage on Extended Cycling for Lithium-Ion BatteriesAIAA Citation: AIAA 2010-6924
2010
-
Dr Matthias GrosseENERGETIXAwardedAward: Effect of a Diaphragm on Performance and Fuel Regression of a Laboratory Scale Hybrid Rocket Motor Using Nitrous Oxide and ParaffinAIAA Citation: AIAA 2009-5113
-
Dr James E PolkJet Propulsion Laboratory (JPL)AwardedAward: Barium Depletion in Hollow Cathode EmittersAIAA Citation: AIAA 2009-5197
-
Mr Adam ButtNASAAwardedAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
-
Andrew K RettenmaierPurdue UniversityAwardedAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
-
Jordan T FarinaVirginia Polytechnic InstituteAwardedAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
-
Bradley C AppelTexas A&M UnivAwardedAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
-
Mr. John TsohasPurdue UniversityAwardedAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
-
Chris PoppNASA-Marshall Space Flight CenterAwardedAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
-
Dr Andrew CortopassiThe Aerospace CorporationAwardedAward: Comparison of Nozzle Throat Erosion Behavior in a Solid Propellant Rocket Motor and a SimulatorAIAA Citation: AIAA 2009-5421
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Mr. Eric BoydPennsylvania State UniversityAwardedAward: Comparison of Nozzle Throat Erosion Behavior in a Solid Propellant Rocket Motor and a SimulatorAIAA Citation: AIAA 2009-5421
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Prof Walter F OBrienVirginia TechAwardedAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
-
Brian J EvansSpace Propulsion Group, Inc.AwardedAward: Comparison of Nozzle Throat Erosion Behavior in a Solid Propellant Rocket Motor and a SimulatorAIAA Citation: AIAA 2009-5421
-
Mr David J SharpJacobs Space Exploration GroupAwardedAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
-
Steve LeperaVA TechAwardedAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
-
Matthew V PerryElectric Jet LLCAwardedAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
-
Dr Stephen D HeisterPurdue UniversityAwardedAward: Development and Launch of the Purdue Hybrid Rocket Technology DemonstratorAIAA Citation: AIAA 2009-4842
-
Dr Uri VandsburgerVPI/SUAwardedAward: Instrumentation, Modeling and Testing of a Gas Turbine Engine Using Lean Premixed Hydrogen CombustionAIAA Citation: AIAA 2009-5048
-
Mr Hank M PittsDynetics, IncAwardedAward: NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design StatusAIAA Citation: AIAA 2009-5130
2007
-
Prof Kimiya KomurasakiThe University of TokyoAwardedAward: Power Transmission to a Micro Aerial VehicleAIAA Citation: AIAA 2007-1003
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Mr. Shuhei KomatsuUniversity of TokyoAwardedAward: Power Transmission to a Micro Aerial VehicleAIAA Citation: AIAA 2007-1003
-
Yoshihiro ArakawaAwardedAward: Power Transmission to a Micro Aerial VehicleAIAA Citation: AIAA 2007-1003
2005
-
Prof S.A. SherifUniversity of FloridaAwardedAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
-
Mr. Robert M ButtonNASA Glenn Research CenterAwardedAward: Distributed, Master-less Control of Modular DC-DC ConvertersAIAA Citation: AIAA 2004-5733
-
David DepoyLockheed Martin CorporationAwardedAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
-
Mr. Thomas D Rahmlow Jr.Rugate Technologies IncAwardedAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
-
Mr. John CrittendenTriad Research Corporation Inc.AwardedAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
-
Dr Jameel KhanUniversity of FloridaAwardedAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
-
Zhiqiang GaoCleveland State UniversityAwardedAward: Distributed, Master-less Control of Modular DC-DC ConvertersAIAA Citation: AIAA 2004-5733
-
Mr. Edward J BrownLockheed Martin CorporationAwardedAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
-
Michael S GrayCleveland State UniversityAwardedAward: Distributed, Master-less Control of Modular DC-DC ConvertersAIAA Citation: AIAA 2004-5733
-
Dr William E LearUniversity of FloridaAwardedAward: Demonstration of a Novel Combined Cooling and Power Gas Turbine with Water HarvestingAIAA Citation: AIAA 2005-0571
-
Mr. Edward GratrixRugate Technologies IncAwardedAward: Thermophotovoltaic Spectral ControlAIAA Citation: AIAA 2004-5762
-
Dr Omar AbdelazizAwardedAward: Air Flow Regimes and Thermal Patterns in Climatized Tombs in Valley of KingsAIAA Citation: AIAA 2005-1444
-
Prof Essam E KhalilCairo UniversityAwardedAward: Air Flow Regimes and Thermal Patterns in Climatized Tombs in Valley of KingsAIAA Citation: AIAA 2005-1444
2004
-
Jorge CamachoUniversity of Texas at El PasoAwardedAward: Characteristics of Nonbuoyant Elliptical Jet Diffusion FlamesAIAA Citation: AIAA 2004-0814
-
Dr WingFai NgTechsburg, Inc.AwardedAward: Thermoelectric Power Generation for UAV ApplicationsAIAA Citation: AIAA 2003-6092
-
Dr Jonathan L FlemingTechsburgAwardedAward: Thermoelectric Power Generation for UAV ApplicationsAIAA Citation: AIAA 2003-6092
-
Dr Ahsan R ChoudhuriUniversity of Texas at El PasoAwardedAward: Characteristics of Nonbuoyant Elliptical Jet Diffusion FlamesAIAA Citation: AIAA 2004-0824