|
Mu-3S-2
|
|
Gross Mass: 13,100 kg (28,800 lb). Empty Mass: 2,800 kg (6,100 lb). Thrust (vac): 523.998 kN (117,799 lbf). Isp: 285 sec. Burn time: 70 sec. Propellants: Solid. Isp(sl): 220 sec. Diameter: 1.41 m (4.62 ft). Span: 1.41 m (4.62 ft). Length: 6.19 m (20.30 ft). Country: Japan. No Engines: 1. Engine: M-23-Mu. Cost $ : 0.430 million. First Flight: 1969. Last Flight: 1995. No Launched: 24. No Failed: 2. Other designations: M-23. 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.
|
|
|
|