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TOS
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Gross Mass: 10,960 kg (24,160 lb). Empty Mass: 1,130 kg (2,490 lb). Thrust (vac): 185.100 kN (41,612 lbf). Isp: 296 sec. Burn time: 144 sec. Propellants: Solid. Isp(sl): 115 sec. Diameter: 2.34 m (7.67 ft). Span: 2.34 m (7.67 ft). Length: 3.29 m (10.79 ft). Country: USA. No Engines: 1. Engine: SRM-1. First Flight: 1982. Last Flight: 1992. No Launched: 19. No Failed: 1. Other designations: Transfer Orbit Stage. IUS-2 stage with simplified electronics.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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