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CD Module
Notional LOx/LH2 rocket engine. Study 1969. CD Modules - conceptual engines of various thrusts, according to design - were clustered in Martin Marietta Nova designs

Status: Study 1969. Thrust: 7,361.00 kN (1,654,818 lbf). Specific impulse: 420 s. Specific impulse sea level: 377 s. Burn time: 397 s.

Used in Nova MM S and T series Nova designs. Status: Study 1963. Operational date would have been July 1978. Values shown were maximum considered.



Country: USA. Launch Vehicles: Nova MM S10E-1, Nova MM S10R-1, Nova MM T10EE-1, Nova MM T10RE-1, Nova MM R10E-2, Nova MM R10R-2, Nova MM S10E-2, Nova MM S10R-2, Nova MM T10RR-2, Nova MM T10RR-3, MLLV. Propellants: Lox/LH2. Stages: Nova MM R10E-2 stage, Nova MM R10R-2 stage, Nova MM S10E-1 stage, Nova MM S10E-2 stage, Nova MM S10R-1 stage, Nova MM S10R-2 stage, Nova MM T10EE-1-1, Nova MM T10EE-1-2, Nova MM T10RE-1-1, Nova MM T10RR-2-1, Nova MM T10RR-3-1, Nova MM T10RR-3-2, MLLV Core.

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