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Engine Model: GEM 60. Designer: Hercules. Gross Mass: 33,199 kg (73,191 lb). Empty Mass: 3,250 kg (7,160 lb). Propellants: Solid. Thrust(vac): 851.500 kN (191,425 lbf). Thrust(sl): 758.000 kN (170,405 lbf). Isp: 275 sec. Isp (sea level): 245 sec. Burn time: 90 sec. Diameter: 1.52 m (4.98 ft). Length: 16.20 m (53.10 ft). Chambers: 1. Chamber Pressure: 90.00 bar. Area Ratio: 11.00. Country: USA. Status: In production. First Flight: 2002. Last Flight: 2002. Flown: 2.00.
GEM 60 used on Rocket Stages
Bibliography:- Isakowitz, Steven J, Hopkins, Joshua B, and Hopkins, Joseph P, International Reference to Space Launch Systems, AIAA, Washington DC, 2004.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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