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1.8KS7800
Part of Sparrow
Multiple-source American solid rocket engine. Sparoair II first stage.

AKA: Mk 6 Mod 3;Sparoair II-1. Status: Retired 1974. Thrust: 35.00 kN (7,868 lbf). Gross mass: 100 kg (220 lb). Burn time: 1.80 s. Height: 1.30 m (4.20 ft). Diameter: 0.20 m (0.65 ft).



Country: USA. Launch Vehicles: Aerobee 300, Sparoair I, Aerobee 300A, Sparoair II, Sparrow Arcas, Sparoair III. Propellants: Solid. Stages: 1.8KS7800.

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