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RO-31
Part of RD-0411 Family
Kosberg nuclear/LH2 rocket engine. UR-700 Third Stage. Study 1967. Engine proposed for UR-700 third stage to achieve 250 metric ton payload to low earth orbit. Probably closely related to RD-0411.

Status: Study 1967. Thrust: 392.00 kN (88,125 lbf).

Propellant Formulation: Nuclear/LH2/Methane.



Family: nuclear-powered. Country: Russia. Launch Vehicles: UR-700 / RO-31. Propellants: Nuclear/LH2. Stages: UR-700-RO-31. Agency: Kosberg bureau. Bibliography: 443.

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