L-5.00H

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Engine Model: L-5.00H. Propellants: Lox/LH2. Thrust(vac): 30,684.000 kN (6,898,037 lbf). Isp: 428 sec. Isp (sea level): 310 sec. Burn time: 500 sec. Chambers: 1. Country: USA. Status: Study 1963. L-5.00H used on Rocket Stages Used on stage: Nova GD-1. on launch vehicle: Nova. 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 - 2008 except where otherwise noted.