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Toroidal 400k
Notional LOx/LH2 rocket engine. Study 1967. Used on Saturn V-3B launch vehicle.

Status: Study 1967. Thrust: 1,778.00 kN (399,710 lbf). Specific impulse: 447 s. Specific impulse sea level: 200 s. Burn time: 385 s.



Country: USA. Launch Vehicles: Saturn V-3B. Propellants: Lox/LH2. Stages: Saturn MS-II-3B, Saturn MS-IVB-3B.

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