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Hopi 3.0KS4000
RPI solid rocket engine.

AKA: 3.0KS4000; Kiva/Hopi-2. Status: Retired 1963. Thrust: 26.40 kN (5,935 lbf). Gross mass: 30 kg (66 lb). Unfuelled mass: 7.00 kg (15.40 lb). Burn time: 3.00 s. Height: 2.10 m (6.80 ft). Diameter: 0.11 m (0.36 ft).

Subtopics

Hopi 2.4KS5600 RPI solid rocket engine.

Hopi 9.0KS1800 RPI solid rocket engine.

Country: USA. Launch Vehicles: Kiva/Hopi. Propellants: Solid. Stages: Hopi 3.0KS4000. Agency: RPI.

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