LS

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Model: LS-A-2. Gross Mass: 300 kg (660 lb). Thrust (vac): 10.000 kN (2,248 lbf). Burn time: 35 sec. Propellants: Solid. Diameter: 0.30 m (0.98 ft). Length: 4.50 m (14.70 ft). Country: Japan. No Engines: 1. Motor: LS-A. Status: Retired 1965. First Flight: 1963. Last Flight: 1965. No Launched: 4. Used as: LS-C. Release conditions: Mitsubishi. Model: LS-C-2. Gross Mass: 300 kg (660 lb). Propellants: Solid. Diameter: 0.60 m (1.96 ft). Length: 4.00 m (13.10 ft). Country: Japan. No Engines: 1. Motor: LS-C. Status: Retired 1974. First Flight: 1968. Last Flight: 1974. No Launched: 8. Used as: LS-C. Release conditions: Mitsubishi. Model: LS-C-1. Gross Mass: 300 kg (660 lb). Propellants: Solid. Diameter: 0.60 m (1.96 ft). Length: 2.50 m (8.20 ft). Country: Japan. No Engines: 1. Motor: LS-C. Status: Retired 1974. First Flight: 1968. Last Flight: 1974. No Launched: 8. Used as: LS-C. Release conditions: Mitsubishi. Used on Launch Vehicles: 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.