5 mlbf Propellants: Lox/LH2. Thrust(vac): 41,361.000 kN (9,298,322 lbf). Isp: 410 sec. Isp (sea level): 345 sec. Burn time: 246 sec. Chambers: 1. Country: USA. Status: Study 1963. First Flight: 1977. 5 mlbf used on Rocket Stages Used on stage: OOST. on launch vehicle: OOST. Used on stage: ROOST. on launch vehicle: ROOST.                   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.

Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z Enter your search terms   Web www.astronautix.com Submit search form