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Toroid FD
Notional LOx/LH2 rocket engine. Study 1963. Operational date would have been December 1976. Engines for recoverable stage. Used on Nova MM T10RR-2 launch vehicle.

Status: Study 1963. Thrust: 20,015.00 kN (4,499,550 lbf). Specific impulse: 455 s. Burn time: 408 s.



Country: USA. Launch Vehicles: Nova MM T10RR-2. Propellants: Lox/LH2. Stages: Nova MM T10RR-2-2.

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