Goldfinch IIA

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Goldfinch IIA

Part of Goldfinch

BAJ solid rocket engine. Skylark 4 first stage.

AKA: Skylark 4-1. Status: Retired 1990. Thrust: 175.00 kN (39,341 lbf). Gross mass: 400 kg (880 lb). Unfuelled mass: 94 kg (207 lb). Burn time: 3.50 s. Height: 2.50 m (8.20 ft). Diameter: 0.44 m (1.44 ft).

Total Impulse: -2 kNs.

Country: UK. Launch Vehicles: Skylark 4, Skylark 4 AC, Skylark 10A, Skylark 12. Propellants: Solid. Stages: Goldfinch IIA. Agency: BAJ.

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