L-7.70

Propellants: Lox/Kerosene. Thrust(vac): 37,007.000 kN (8,319,504 lbf). Isp: 335 sec. Isp (sea level): 310 sec. Burn time: 203 sec. Chambers: 1. Country: USA. Status: Study 1963.

Engines used in recoverable stage; separation at 3,365 m/s at 89,300 m altitude; splashdown using retrorockets under 8 46 m diameter parachutes 1300 km downrange.

L-7.70 used on Rocket Stages

Used on stage: Nova GD-F-1. on launch vehicle: Nova GD-F.

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