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K250-8
Part of K250-300
ISAS solid rocket engine. Kappa 8 second stage.

AKA: Kappa 8-2. Status: Retired 1970. Thrust: 34.00 kN (7,643 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 50 kg (110 lb). Burn time: 9.70 s. Height: 3.10 m (10.10 ft). Diameter: 0.25 m (0.82 ft).



Country: Japan. Launch Vehicles: Kappa 8. Propellants: Solid. Stages: K250-8. Agency: ISAS.

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