HP-1

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HP-1

Notional LOx/LH2 rocket engine. Study 1963. Operational date would have been December 1974. Used in Martin Nova studies MM 24G, MM 33.

Status: Study 1963. Thrust: 6,536.00 kN (1,469,351 lbf). Specific impulse: 451 s. Specific impulse sea level: 379 s. Burn time: 386 s.

Country: USA. Launch Vehicles: Nova MM 33, Nova MM 24G. Propellants: Lox/LH2. Stages: Nova MM 24G-2, Nova MM 33-1, Nova MM-1.

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