NERVA/Lox Mixed Cycle Propellants: Nuclear/LH2. Thrust(vac): 24,126.000 kN (5,423,740 lbf). Isp: 810 sec. Isp (sea level): 410 sec. Burn time: 285 sec. Chambers: 1. Country: USA. Status: Study 1963. NERVA/Lox Mixed Cycle used on Rocket Stages Used on stage: RITA C. on launch vehicle: RITA C.                   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.

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