|
H-1-1
|
|
Gross Mass: 85,800 kg (189,100 lb). Empty Mass: 4,400 kg (9,700 lb). Thrust (vac): 866.710 kN (194,844 lbf). Isp: 290 sec. Burn time: 270 sec. Propellants: Lox/Kerosene. Isp(sl): 253 sec. Diameter: 2.44 m (8.00 ft). Span: 2.44 m (8.00 ft). Length: 22.00 m (72.00 ft). Country: Japan. No Engines: 1. Engine: MB-3-3. Cost $ : 30.000 million. First Flight: 1986. Last Flight: 1992. No Launched: 9. Other designations: Extended Length Tank Thor MB-3. License built MB-3 ELT Thor 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.
|
|
|
|