Goose II (original) (raw)

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Goose II

RO solid rocket engine. INTA-255 first stage.

AKA: INTA-255-1. Status: Retired 1970. Thrust: 22.00 kN (4,945 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 95 kg (209 lb). Burn time: 17 s. Height: 3.40 m (11.10 ft). Diameter: 0.26 m (0.85 ft).

Country: UK. Launch Vehicles: INTA-255. Propellants: Solid. Stages: Goose II. Agency: RO.

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