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K250-300
Thrust: 43.00 kN (9,666 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 50 kg (110 lb). Burn time: 7.60 s. Height: 4.60 m (15.00 ft). Diameter: 0.25 m (0.82 ft).
| K250H ISAS solid rocket engine. Kappa 8L first stage. |
| K250-8 ISAS solid rocket engine. Kappa 8 second stage. |
Country: Japan. Propellants: Solid. Agency: ISAS.
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