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SO-250

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SO-250
Part of K250-200 Family
ISAS solid rocket engine. S-250 first stage.

AKA: S-250-1. Status: Retired 1969. Gross mass: 200 kg (440 lb). Height: 2.00 m (6.50 ft). Diameter: 0.25 m (0.82 ft).

Country: Japan. Launch Vehicles: S-250. Propellants: Solid. Stages: SO-250. Agency: ISAS.



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