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RD-0411
Kosberg nuclear/LH2 rocket engine. Full-size nuclear thermal engine. Design concept 1965-94. Planned full-size nuclear thermal engine for Mars expeditions. Never progressed beyond study stage.

Status: Design concept 1965-94. Date: 1965-94. Thrust: 392.00 kN (88,125 lbf). Specific impulse: 900 s.



Subtopics

RO-31 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.

Family: nuclear-powered. Country: Russia. Propellants: Nuclear/LH2. Agency: Kosberg bureau. Bibliography: 307, 95.

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