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Gosling 4

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Gosling 4
Part of Gosling stage Family
RO solid rocket engine. Skylark 10A second stage, INTA-300 first stage.

AKA: INTA-300-1; Skylark 10A-2. Status: Retired 1974. Thrust: 137.00 kN (30,798 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 72 kg (158 lb). Burn time: 3.10 s. Height: 3.60 m (11.80 ft). Diameter: 0.26 m (0.85 ft).

Country: UK. Launch Vehicles: INTA-300, Skylark 10A, Fulmar, INTA-300B. Propellants: Solid. Stages: Gosling 4. Agency: RO.



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