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Nuclear 12 Gw
Notional nuclear/LH2 rocket engine. Helios A, Helios C study 1960. Nuclear second stage.

Status: Study 1960. Thrust: 2,892.00 kN (650,147 lbf). Specific impulse: 830 s. Burn time: 355 s.



Family: nuclear-powered. Country: USA. Launch Vehicles: Helios A, Helios C. Propellants: Nuclear/LH2. Stages: Helios A-2, Helios C-2.

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