Titan Transtage

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Titan Transtage

N2O4/Aerozine-50 propellant rocket stage, originally developed for the Titan 3C / Dynasoar, continued after Dynasoar's cancellation. Flown 1968-1982 on Titan 3A and 3C boosters. Transtage mass indicated was that remaining after insertion of Dynasoar and Abort Stage into orbit. Transtage had its own RCS. Maneuver in earth orbit.

AKA: Transtage. Status: Out of production. Thrust: 71.17 kN (15,999 lbf). Gross mass: 12,247 kg (27,000 lb). Unfuelled mass: 1,950 kg (4,290 lb). Specific impulse: 311 s. Burn time: 440 s. Height: 4.57 m (14.99 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 14.500 million. No Engines: 2.

More at: Titan Transtage.

Subtopics

Transtage 1, 2, 5 Instrumented third stage satellite, USA. Launched 1964 - 1965.

Titan Transtage Stretch N2O4/Aerozine-50 propellant rocket stage. 20% stretch of Transtage to handle geosynchronous insertion of larger payloads launched by Titan 3C7. Masses estimated.

OV4 3 Experimental satellite built by Martin Marietta for USAF, USA. Launched 1966. Used the Transtage bus.

Family: Space Tugs. Country: USA. Engines: AJ10-138. Spacecraft: Dynasoar. Launch Vehicles: Titan IIIC, Titan IIIA, Titan 23C, Titan 34D/Transtage. Propellants: N2O4/Aerozine-50, N2O4/UDMH.

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