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Kappa 1 engine
ISAS solid rocket engine. Kappa 3 second stage.

AKA: Kappa 1;Kappa 3-2. Status: Retired 1957. Number: 1 . Thrust: 10.00 kN (2,248 lbf). Unfuelled mass: 20 kg (44 lb). Burn time: 3.00 s. Height: 2.70 m (8.80 ft). Diameter: 0.13 m (0.42 ft).



Country: Japan. Launch Vehicles: Kappa 1, Kappa 2, Kappa 3. Propellants: Solid. Stages: Kappa 1 engine. Agency: ISAS.

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