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DAC Helios-1
Part of DAC Helios Family
LOx/LH2 propellant rocket stage. .

Status: Study 1963. Thrust: 52,926.00 kN (11,898,238 lbf). Gross mass: 1,660,000 kg (3,650,000 lb). Unfuelled mass: 149,000 kg (328,000 lb). Specific impulse: 410 s. Specific impulse sea level: 345 s. Burn time: 113 s. Height: 16.20 m (53.10 ft). Diameter: 24.40 m (80.00 ft). Span: 29.00 m (95.00 ft).

No Engines: 4.



Country: USA. Engines: Chamber/single nozzle. Launch Vehicles: DAC Helios. Propellants: Lox/LH2.

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