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DAC Helios ISI-1
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Gross Mass: 1,333,000 kg (2,938,000 lb). Empty Mass: 120,000 kg (260,000 lb). Thrust (vac): 49,807.000 kN (11,197,059 lbf). Isp: 455 sec. Burn time: 107 sec. Propellants: Lox/LH2. Isp(sl): 365 sec. Diameter: 24.40 m (80.00 ft). Span: 29.00 m (95.00 ft). Length: 22.90 m (75.10 ft). Country: USA. No Engines: 4. Engine: Chamber/single nozzle. Status: Study 1963. Cost $ : 38.700 million.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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