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M14
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Designer: Nissan. Gross Mass: 83,560 kg (184,210 lb). Empty Mass: 12,070 kg (26,600 lb). Propellants: Solid. Thrust(vac): 3,780.300 kN (849,845 lbf). Thrust(sl): 3,369.400 kN (757,471 lbf). Isp: 276 sec. Isp (sea level): 246 sec. Burn time: 46 sec. Diameter: 2.50 m (8.20 ft). Length: 13.80 m (45.20 ft). Chambers: 1. Chamber Pressure: 59.00 bar. Area Ratio: 11.00. Country: Japan. First Flight: 1997. Last Flight: 2006. Flown: 7.00.
M14 used on Rocket Stages - Used on stage: M-V-1. on launch vehicle: M-V.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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