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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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