Star 27

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Model: OIS. Gross Mass: 361 kg (795 lb). Empty Mass: 27 kg (59 lb). Thrust (vac): 27.000 kN (6,069 lbf). Burn time: 34 sec. Propellants: Solid. Diameter: 0.69 m (2.26 ft). Length: 1.20 m (3.90 ft). Country: USA. No Engines: 1. Motor: Star 27. Status: Retired 1985. First Flight: 1979. Last Flight: 1985. No Launched: 2. Used as: Star 27. Release conditions: Fairchild. Model: Star 27. Gross Mass: 361 kg (795 lb). Empty Mass: 27 kg (59 lb). Thrust (vac): 27.000 kN (6,069 lbf). Burn time: 34 sec. Propellants: Solid. Diameter: 0.69 m (2.26 ft). Length: 1.20 m (3.90 ft). Country: USA. No Engines: 1. Motor: Star 27. Status: Retired 1991. First Flight: 1988. Last Flight: 1991. No Launched: 3. Used as: Star 27. Release conditions: Thiokol. Used on Launch Vehicles: Atlas. Strypi. 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.