NAL

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Model: NAL-16-1. Gross Mass: 100 kg (220 lb). Empty Mass: 40 kg (88 lb). Thrust (vac): 10.000 kN (2,248 lbf). Burn time: 14 sec. Propellants: Solid. Diameter: 0.17 m (0.54 ft). Length: 3.90 m (12.70 ft). Country: Japan. No Engines: 1. Motor: NAL-16. Status: Retired 1969. First Flight: 1965. Last Flight: 1969. No Launched: 5. Used as: STA S. Release conditions: Mitsubishi. Model: NAL-25-1. Propellants: Solid. Diameter: 0.25 m (0.82 ft). Length: 4.00 m (13.10 ft). Country: Japan. No Engines: 1. Motor: NAL-25. Status: Retired 1969. First Flight: 1969. Last Flight: 1969. No Launched: 1. Used as: STA S. Release conditions: Mitsubishi. Model: NAL-7-1. Propellants: Solid. Diameter: 0.0700 m (0.2290 ft). Length: 2.00 m (6.50 ft). Country: Japan. No Engines: 1. Motor: NAL-7. Status: Retired 1970. First Flight: 1969. Last Flight: 1970. No Launched: 2. 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.