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Nuclear 14 Gw
Notional nuclear/LH2 rocket engine. Study 1960. Nuclear second stage Used on Helios B launch vehicle.

Status: Study 1960. Thrust: 3,334.00 kN (749,513 lbf). Specific impulse: 830 s. Burn time: 355 s.



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

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