| Astrorocket-1 |
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Model: Astrorocket-1. Gross Mass: 981,859 kg (2,164,628 lb). Empty Mass: 132,000 kg (291,000 lb). Thrust (vac): 14,700.000 kN (3,304,600 lbf). Isp: 293 sec. Burn time: 164 sec. Propellants: N2O4/Aerozine-50. Isp(sl): 258 sec. Diameter: 7.00 m (22.90 ft). Span: 40.00 m (131.00 ft). Length: 65.00 m (213.00 ft). Country: USA. No Engines: 9. Status: Study 1962. Cost $ : 18.000 million. First Flight: 1973. Delta wing configuration. LR87-derivative engines. Used on Launch Vehicles: 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. |