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K160
Part of S-160
ISAS solid rocket engine. Kappa 8L second stage.

AKA: Kappa 8L-2. Status: Retired 1966. Gross mass: 100 kg (220 lb). Unfuelled mass: 20 kg (44 lb). Burn time: 5.30 s. Height: 2.40 m (7.80 ft). Diameter: 0.16 m (0.52 ft).

Country: Japan. Launch Vehicles: Kappa 8L. Propellants: Solid. Stages: K160. Agency: ISAS.
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