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K250H
Part of K250-300 Family
ISAS solid rocket engine. Kappa 8L first stage.

AKA: Kappa 8L-1. Status: Retired 1966. Gross mass: 300 kg (660 lb). Unfuelled mass: 50 kg (110 lb). Burn time: 7.20 s. Height: 3.60 m (11.80 ft). Diameter: 0.25 m (0.82 ft).



Country: Japan. Launch Vehicles: Kappa 6H, Kappa 8L. Propellants: Solid. Stages: K250H. Agency: ISAS.

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