Hopi 2.4KS5600 (original) (raw)

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Hopi 2.4KS5600

Part of Hopi 3.0KS4000

RPI solid rocket engine.

AKA: 2.4KS5600;Hopi III. Status: Retired 1964. Thrust: 28.00 kN (6,294 lbf). Gross mass: 30 kg (66 lb). Unfuelled mass: 8.00 kg (17.60 lb). Burn time: 2.10 s. Height: 2.00 m (6.50 ft). Diameter: 0.11 m (0.36 ft).

Country: USA. Launch Vehicles: Hopi Dart. Propellants: Solid. Stages: Hopi 2.4KS5600. Agency: RPI.

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