K420H

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K420H

Part of K420

ISAS solid rocket engine. Kappa 10S first stage.

AKA: Kappa 10S-1. Status: Retired 1988. Thrust: 110.00 kN (24,720 lbf). Gross mass: 1,200 kg (2,600 lb). Unfuelled mass: 200 kg (440 lb). Burn time: 17 s. Height: 5.80 m (19.00 ft). Diameter: 0.42 m (1.37 ft).

Country: Japan. Launch Vehicles: Kappa 9M, Kappa 10S, Kappa 10, Kappa 10C. Propellants: Solid. Stages: K420H. Agency: ISAS.

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