NERVA 1mlbf

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NERVA 1mlbf

Notional nuclear/LH2 rocket engine. DAC Helios, DAC Helios ISI studies 1963.

Status: Study 1963. Thrust: 8,963.00 kN (2,014,962 lbf). Specific impulse: 850 s. Burn time: 392 s.

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

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