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OAM
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Gross Mass: 714 kg (1,574 lb). Empty Mass: 360 kg (790 lb). Thrust (vac): 882 N (198 lbf). Isp: 222 sec. Burn time: 1,500 sec. Propellants: Hydrazine. Diameter: 2.30 m (7.50 ft). Span: 2.30 m (7.50 ft). Length: 1.00 m (3.20 ft). Country: USA. No Engines: 4. Engine: MR-107. Status: Out of production. First Flight: 1995. Last Flight: 2001. No Launched: 7. Monopropellant final stage providing precise orbital injection. Pressure-fed, indefinite number of restarts.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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