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Model: Titan Transtage. Gross Mass: 12,247 kg (27,000 lb). Empty Mass: 1,950 kg (4,290 lb). Thrust (vac): 71.166 kN (15,999 lbf). Isp: 311 sec. Burn time: 440 sec. Propellants: N2O4/Aerozine-50. Isp(sl): 0 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 4.57 m (14.99 ft). Country: USA. No Engines: 2. Motor: AJ10-138. Status: Out of production. Cost $ : 14.500 million. First Flight: 1959. Last Flight: 1989. No Launched: 130. No Failed: 4. Other designations: Transtage.
Model: Titan Transtage Stretch. Gross Mass: 15,000 kg (33,000 lb). Empty Mass: 2,200 kg (4,800 lb). Thrust (vac): 71.166 kN (15,999 lbf). Isp: 311 sec. Burn time: 520 sec. Propellants: N2O4/Aerozine-50. Isp(sl): 0 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 5.30 m (17.30 ft). Country: USA. No Engines: 2. Motor: AJ10-138. Status: Study 1965. Cost $ : 15.000 million. 20% stretch of Transtage to handle geosynch insertion of larger payloads launched by Titan 3C7. Masses estimated. Used on Launch Vehicles: 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. |