Falcon
Falcon 9 Launch
Falcon Heavy Launch
About SpaceX
SpaceX was founded by Elon Musk, who became wealthy as an Internet entrepreneur. A native of South Africa, Musk dropped out of Stanford in 1995 to found Zip2, which was sold in 1999 for $300 million. His second company, PayPal, was sold to eBay for $1.5 billion in 2002. Early in 2002, Musk assembled a team of people experienced with the space launch industry to study whether it was possible to build a low-cost launch vehicle in a developed country with high labor costs. The results of the study were positive, and so Musk founded Space Exploration Technologies (SpaceX) in June 2002. He hired a few dozen managers and engineers from established aerospace companies to build the Falcon launch vehicle. Development has progressed rapidly, with first launch planned in 2004.
Falcon Vehicle Descriptions
Falcon 9
General Description
National Origin
United StatesMain Organization
Summary
Flight Rate
Estimated Launch Price
Falcon 9: $62 million plus range and payload specific costs (SpaceX, 2020)
Spaceports
CAPE CANAVERAL AIR FORCE STATION, FLORIDA
KENNEDY SPACE CENTER, FLORIDA
VANDENBERG AIR FORCE BASE, CALIFORNIA
Primary Missions
Medium to heavy payloads to LEO
Status
Key Organizations
Marketing Organization
Launch Service Provider
Prime Contractor
Performance
Falcon 9 | |
200 km (108 nmi) at 28.5° 200 km (108 nmi) at 90° |
22,800 kg |
Space Station orbit: 407 km (220 nmi), 51.6° Sun-synchronous orbit: 800 km (432 nmi), 98.6° |
22,800 kg (50,265 lb) |
GTO: 108 ´ 35,786 km (100 nmi ´ 19,323), 27° | 8,300 kg (18,300 lb) |
Mars | 4,020 kg (8860 lb) |
Pluto |
* Performance represents max capability on fully expendable vehicle
Falcon Heavy
General Description
National Origin
United StatesMain Organization
Summary
Flight Rate
Estimated Launch Price
Falcon Heavy $90 million plus range and payload specific costs (SpaceX, 2020)
Primary Missions
Medium to heavy payloads to LEO
Status
Key Organizations
Marketing Organization
Launch Service Provider
Prime Contractor
Performance
Falcon Heavy | |
200 km (108 nmi) at 28.5° 200 km (108 nmi) at 90° |
63,800 kg |
Space Station orbit: 407 km (220 nmi), 51.6° Sun-synchronous orbit: 800 km (432 nmi), 98.6° |
63,800 kg (140,660 lb) |
GTO: 108 ´ 35,786 km (100 nmi ´ 19,323), 27° | 26,700 kg (58,860 lb) |
Mars | 16,800 kg (37,040 lb) |
Pluto | 3,500 kg |
* Performance represents max capability on fully expendable vehicle