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K250-100
Thrust: 34.00 kN (7,643 lbf). Gross mass: 100 kg (220 lb). Unfuelled mass: 40 kg (88 lb). Burn time: 9.30 s. Height: 1.00 m (3.20 ft). Diameter: 0.25 m (0.82 ft).
| K245-1 Solid rocket stage. 34.00 kN (7,644 lbf) thrust. Mass 100 kg (220 lb). |
| NAL-25 engine Mitsubishi solid rocket engine. NAL-25 first stage. |
Country: Japan. Propellants: Solid. Agency: ISAS.
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