L500

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Engine Model: L500. Designer: ISAS. Gross Mass: 800 kg (1,760 lb). Propellants: Solid. Thrust(vac): 69.000 kN (15,511 lbf). Burn time: 27 sec. Diameter: 0.50 m (1.64 ft). Length: 2.50 m (8.20 ft). Country: Japan. L500 used on Rocket Stages Used on stage: L500. on launch vehicle: Lambda. 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.