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Helios Stage 1
Notional LOx/LH2 rocket engine. Study 1960. Engines for booster stage with LOx tanks only to take nuclear second stage to stratosphere. Helios A, B, C studies.

Status: Study 1960. Thrust: 1,667.00 kN (374,756 lbf). Specific impulse: 400 s. Specific impulse sea level: 340 s. Burn time: 117 s.



Country: USA. Launch Vehicles: Helios A, Helios B, Helios C. Propellants: Lox/LH2. Stages: Helios A-1, Helios B-1, Helios C-1.

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