Orion 50

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Model: Orion 50. Gross Mass: 3,370 kg (7,420 lb). Empty Mass: 345 kg (760 lb). Thrust (vac): 118.199 kN (26,572 lbf). Isp: 292 sec. Burn time: 73 sec. Propellants: Solid. Isp(sl): 240 sec. Diameter: 1.27 m (4.16 ft). Span: 1.27 m (4.16 ft). Length: 2.65 m (8.69 ft). Country: USA. No Engines: 1. Motor: Pegasus-2. Status: Active. Cost $ : 3.000 million. First Flight: 1990. Last Flight: 2007. No Launched: 58. Model: Pegasus XL-2. Gross Mass: 4,331 kg (9,548 lb). Empty Mass: 416 kg (917 lb). Thrust (vac): 153.503 kN (34,509 lbf). Isp: 290 sec. Burn time: 73 sec. Propellants: Solid. Isp(sl): 240 sec. Diameter: 1.27 m (4.16 ft). Span: 1.27 m (4.16 ft). Length: 3.58 m (11.74 ft). Country: USA. No Engines: 1. Motor: Pegasus XL-2. Status: Active. Cost $ : 3.400 million. First Flight: 1994. Last Flight: 2007. No Launched: 92. No Failed: 1. Used on Launch Vehicles: Minotaur. OBV. Pegasus. Taurus. 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.