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Engine Model: Goose II. Designer: RO. Gross Mass: 300 kg (660 lb). Empty Mass: 95 kg (209 lb). Propellants: Solid. Thrust(vac): 22.000 kN (4,945 lbf). Burn time: 17 sec. Diameter: 0.26 m (0.85 ft). Length: 3.40 m (11.10 ft). Country: UK.



Goose used on Rocket Stages


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