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Snipe
RO solid rocket engine. Fulmar second stage.

AKA: Fulmar-2. Status: Retired 1994. Thrust: 16.00 kN (3,596 lbf). Gross mass: 200 kg (440 lb). Unfuelled mass: 58 kg (127 lb). Burn time: 16 s. Height: 2.10 m (6.80 ft). Diameter: 0.26 m (0.85 ft).



Country: UK. Launch Vehicles: INTA-300, Fulmar, INTA-300B. Propellants: Solid. Stages: Snipe. Agency: RO.

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