Engine Model: CD Module. Propellants: Lox/LH2. Thrust(vac): 7,361.000 kN (1,654,818 lbf). Isp: 420 sec. Isp (sea level): 377 sec. Burn time: 397 sec. Chambers: 1. Country: USA. Status: Study 1969. CD Modules - conceptual engines of various thrusts, according to design - were clustered in Martin Marietta Nova designs. 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.
CD Module used on Rocket Stages
- Used on stage: MLLV. on launch vehicle: MLLV.