Kappa 1

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Engine Model: Kappa 1. Designer: ISAS. Empty Mass: 20 kg (44 lb). Propellants: Solid. Thrust(vac): 10.000 kN (2,248 lbf). Burn time: 3.00 sec. Diameter: 0.13 m (0.42 ft). Length: 2.70 m (8.80 ft). Country: Japan. Kappa 1 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.