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Hyperion Sustainer
Part of Hyperion Family
Nuclear/LH2 propellant rocket stage. .

Status: Study 1959. Thrust: 5,782.68 kN (1,299,998 lbf). Gross mass: 453,592 kg (999,999 lb). Unfuelled mass: 110,000 kg (240,000 lb). Specific impulse: 800 s. Burn time: 460 s. Height: 51.00 m (167.00 ft). Diameter: 8.54 m (28.01 ft). Span: 8.54 m (28.01 ft).

No Engines: 2.



Country: USA. Engines: Nerva 12 GW. Launch Vehicles: Hyperion 1958. Propellants: Nuclear/LH2.

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