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Engine Model: Hopi 2.4KS5600. Other Designations: 2.4KS5600. Designer: RPI. Gross Mass: 30 kg (66 lb). Empty Mass: 8.00 kg (17.60 lb). Propellants: Solid. Thrust(vac): 28.000 kN (6,294 lbf). Burn time: 2.10 sec. Diameter: 0.11 m (0.36 ft). Length: 2.00 m (6.50 ft). Country: USA.



Hopi 2.4KS5600 used on Rocket Stages

  • Used on stage: Hopi. on launch vehicle: Raven.

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