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Engine Model: M-V-4. Designer: Nissan. Gross Mass: 1,430 kg (3,150 lb). Empty Mass: 118 kg (260 lb). Propellants: Solid. Thrust(vac): 52.000 kN (11,690 lbf). Isp: 298 sec. Burn time: 73 sec. Diameter: 1.20 m (3.90 ft). Length: 1.50 m (4.90 ft). Chambers: 1. Chamber Pressure: 49.00 bar. Area Ratio: 89.00. Country: Japan. First Flight: 1997. Last Flight: 2006. Flown: 7.00.
M-V-4 used on Rocket Stages - Used on stage: K420. on launch vehicle: Kappa.
- Used on stage: K420. on launch vehicle: M-V.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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