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22.6KS1245
Multiple-source American solid rocket engine. Sparoair III second stage.

AKA: Sparoair III-2;Sparrow engine. Status: Retired 1966. Thrust: 5.50 kN (1,236 lbf). Gross mass: 100 kg (220 lb). Burn time: 23 s. Height: 1.30 m (4.20 ft). Diameter: 0.20 m (0.65 ft).

Country: USA. Launch Vehicles: Sparoair III. Propellants: Solid. Stages: 22.6KS1245.
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