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IABS
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Gross Mass: 1,578 kg (3,478 lb). Empty Mass: 275 kg (606 lb). Thrust (vac): 980 N (220 lbf). Isp: 312 sec. Burn time: 60 sec. Propellants: N2O4/MMH. Isp(sl): 0 sec. Diameter: 2.90 m (9.50 ft). Span: 2.90 m (9.50 ft). Length: 0.68 m (2.23 ft). Country: USA. No Engines: 2. Engine: R-4D. Status: Out of production. Cost $ : 15.000 million. First Flight: 1991. Last Flight: 1998. No Launched: 10. Other designations: Integrated Apogee Boost Subsystem.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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