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K250-200
Thrust: 34.00 kN (7,643 lbf). Gross mass: 200 kg (440 lb). Unfuelled mass: 40 kg (88 lb). Burn time: 9.30 s. Height: 2.30 m (7.50 ft). Diameter: 0.25 m (0.82 ft).
| SO-250 ISAS solid rocket engine. S-250 first stage. |
Country: Japan. Propellants: Solid. Agency: ISAS.
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