S-A

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Model: S-A-1. Gross Mass: 100 kg (220 lb). Propellants: Solid. Diameter: 0.16 m (0.52 ft). Length: 2.80 m (9.10 ft). Country: Japan. No Engines: 1. Motor: S-A. Status: Retired 1963. First Flight: 1963. Last Flight: 1963. No Launched: 3. Used as: STA S. Release conditions: Mitsubishi. Model: SA-II-1. Propellants: Solid. Diameter: 0.10 m (0.32 ft). Length: 1.00 m (3.20 ft). Country: Japan. No Engines: 1. Motor: SA-II. Status: Retired 1968. First Flight: 1968. Last Flight: 1968. No Launched: 1. Used as: STA S. Release conditions: Mitsubishi. Used on Launch Vehicles: S. 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.