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Engine Model: S-310. Designer: ISAS. Gross Mass: 600 kg (1,320 lb). Propellants: Solid. Diameter: 0.31 m (1.01 ft). Length: 6.00 m (19.60 ft). Country: Japan.
Engine Model: SB-310. Designer: ISAS. Gross Mass: 500 kg (1,100 lb). Empty Mass: 190 kg (410 lb). Propellants: Solid. Thrust(vac): 95.000 kN (21,356 lbf). Burn time: 7.40 sec. Diameter: 0.31 m (1.01 ft). Length: 5.80 m (19.00 ft). Country: Japan.
S-310 used on Rocket Stages - Used on stage: S-310. on launch vehicle: S.
- Used on stage: SB-310. on launch vehicle: Mu.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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