5.6KS5400

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5.6KS5400

Part of Viper-27

Multiple-source American solid rocket engine. Nike Viper I second stage.

AKA: Nike Viper I-2. Status: Retired 1960. Thrust: 24.00 kN (5,395 lbf). Gross mass: 90 kg (198 lb). Unfuelled mass: 25 kg (55 lb). Burn time: 5.60 s. Height: 2.70 m (8.80 ft). Diameter: 0.17 m (0.54 ft).

Country: USA. Launch Vehicles: ALSOR, Nike Viper I, Viper Falcon. Propellants: Solid. Stages: 5.6KS5400.

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