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Engine Model: K250. Designer: ISAS. Gross Mass: 300 kg (660 lb). Empty Mass: 50 kg (110 lb). Propellants: Solid. Thrust(vac): 43.000 kN (9,666 lbf). Burn time: 7.60 sec. Diameter: 0.25 m (0.82 ft). Length: 4.60 m (15.00 ft). Country: Japan.
Engine Model: K250-8. Designer: ISAS. Gross Mass: 300 kg (660 lb). Empty Mass: 50 kg (110 lb). Propellants: Solid. Thrust(vac): 34.000 kN (7,643 lbf). Burn time: 9.70 sec. Diameter: 0.25 m (0.82 ft). Length: 3.10 m (10.10 ft). Country: Japan.
Engine Model: K250H. Designer: ISAS. Gross Mass: 300 kg (660 lb). Empty Mass: 50 kg (110 lb). Propellants: Solid. Burn time: 7.20 sec. Diameter: 0.25 m (0.82 ft). Length: 3.60 m (11.80 ft). Country: Japan.
Engine Model: SO-250. Designer: ISAS. Gross Mass: 200 kg (440 lb). Propellants: Solid. Diameter: 0.25 m (0.82 ft). Length: 2.00 m (6.50 ft). Country: Japan.
K250 used on Rocket Stages - Used on stage: K245. on launch vehicle: Kappa.
- Used on stage: K250. on launch vehicle: Kappa.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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