Kappa 4 Booster

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Engine Model: Kappa 4 Booster. Designer: ISAS. Propellants: Solid. Thrust(vac): 105.000 kN (23,604 lbf). Burn time: 3.00 sec. Diameter: 0.33 m (1.08 ft). Length: 3.30 m (10.80 ft). Country: Japan. Kappa 4 Booster used on Rocket Stages Used on stage: Kappa. on launch vehicle: Kappa. 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.