Delta P Gross Mass: 5,434 kg (11,979 lb). Empty Mass: 820 kg (1,800 lb). Thrust (vac): 41.923 kN (9,425 lbf). Isp: 301 sec. Burn time: 322 sec. Propellants: N2O4/Aerozine-50. Isp(sl): 0 sec. Diameter: 1.38 m (4.52 ft). Span: 1.38 m (4.52 ft). Length: 5.97 m (19.58 ft). Country: USA. No Engines: 1. Engine: TR-201. Cost $ : 4.350 million. First Flight: 1972. Last Flight: 1989. No Launched: 90. No Failed: 1. Other designations: TR-201. Used on Launch Vehicles: Delta 1000. Delta 2000. Delta 3000.                   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 - 2007 except where otherwise noted.

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