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Engine Model: Hopi 3.0KS4000. Other Designations: 3.0KS4000. Designer: RPI. Gross Mass: 30 kg (66 lb). Empty Mass: 7.00 kg (15.40 lb). Propellants: Solid. Thrust(vac): 18.000 kN (4,046 lbf). Burn time: 3.00 sec. Diameter: 0.11 m (0.36 ft). Length: 2.10 m (6.80 ft). Country: USA.

Hopi 3.0KS4000 used on Rocket Stages
  • Used on stage: Hopi. on launch vehicle: Raven.
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