|
X-34
|
|
Gross Mass: 21,800 kg (48,000 lb). Empty Mass: 8,200 kg (18,000 lb). Thrust (vac): 268.927 kN (60,457 lbf). Isp: 310 sec. Burn time: 150 sec. Propellants: Lox/Kerosene. Span: 8.54 m (28.01 ft). Length: 17.68 m (58.00 ft). Country: USA. No Engines: 1. Engine: Fastrac. Status: Development ended 1996. First Flight: 2000. Low cost reusable vehicle technology demonstrator.
Used on Launch Vehicles:
|
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2007 except where otherwise noted.
|
|
|
|