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Kappa 9L-1
Solid rocket stage. 110.00 kN (24,729 lbf) thrust. Mass 1,200 kg (2,646 lb).

Status: Retired 1970. 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 7, Kappa 8, Kappa 9L. Propellants: Solid. Agency: ISAS.

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