Kisha I 4.4KS4800

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Engine Model: Kisha I 4.4KS4800. Other Designations: 4.4KS4800. Designer: PRI. Gross Mass: 100 kg (220 lb). Propellants: Solid. Thrust(vac): 21.000 kN (4,720 lbf). Burn time: 4.40 sec. Diameter: 0.17 m (0.55 ft). Length: 2.00 m (6.50 ft). Country: USA. Kisha I 4.4KS4800 used on Rocket Stages Used on stage: Kisha. on launch vehicle: Cajun. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.