Hyperion Booster

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Model: Hyperion Booster. Gross Mass: 394,625 kg (869,999 lb). Empty Mass: 18,144 kg (40,000 lb). Thrust (vac): 13,700.000 kN (3,079,800 lbf). Isp: 457 sec. Burn time: 70 sec. Propellants: Lox/LH2. Isp(sl): 365 sec. Diameter: 8.54 m (28.01 ft). Span: 13.00 m (42.00 ft). Length: 12.00 m (39.00 ft). Country: USA. No Engines: 4. Status: Study 1959. Used on Launch Vehicles: Hyperion 1958. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.