Raven 8

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Raven 8

Part of Rook engine

RO solid rocket engine. Skylark 4 second stage.

AKA: Skylark 4-2. Status: Retired 1989. Thrust: 50.10 kN (11,263 lbf). Gross mass: 1,100 kg (2,400 lb). Unfuelled mass: 230 kg (500 lb). Burn time: 30 s. Height: 5.40 m (17.70 ft). Diameter: 0.44 m (1.44 ft).

Country: UK. Launch Vehicles: Skylark 2, Skylark 2 AC, Skylark 4, Skylark 4 AC. Propellants: Solid. Stages: Raven 8. Agency: RO.

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