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M24
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Designer: Nissan. Gross Mass: 34,470 kg (75,990 lb). Empty Mass: 3,410 kg (7,510 lb). Propellants: Solid. Thrust(vac): 1,245.300 kN (279,955 lbf). Thrust(sl): 877.700 kN (197,315 lbf). Isp: 288 sec. Isp (sea level): 203 sec. Burn time: 71 sec. Diameter: 2.50 m (8.20 ft). Length: 6.80 m (22.30 ft). Chambers: 1. Chamber Pressure: 59.00 bar. Area Ratio: 31.00. Country: Japan. First Flight: 1997. Last Flight: 2006. Flown: 7.00.
M24 used on Rocket Stages - Used on stage: M-V-2. on launch vehicle: M-V.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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