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Titan IIIA
Part of Titan
Titan 3A
Titan 3A
Titan 3A - COSPAR 1965-008
American orbital launch vehicle. Titan with Transtage third stage. Core for Titan 3C.

AKA: SLV-5A;Titan 3A. Status: Retired 1965. First Launch: 1964-09-01. Last Launch: 1965-05-06. Number: 4 . Payload: 3,100 kg (6,800 lb). Thrust: 1,936.90 kN (435,432 lbf). Gross mass: 161,730 kg (356,550 lb). Height: 42.00 m (137.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 3,100 kg (6,800 lb) to a 185 km orbit. Flyaway Unit Cost 1985$: 30.740 million.

Stage Data - Titan 3A



Family: orbital launch vehicle. Country: USA. Engines: AJ10-138, LR87-11, LR91-11. Spacecraft: LES, LCS. Launch Sites: Cape Canaveral, Cape Canaveral LC20. Stages: Titan 3A-1, Titan 3A-2, Titan Transtage. Agency: Martin.
Photo Gallery

Titan 3ATitan 3A
Credit: © Mark Wade


Titan LVs SmallTitan LVs Small
Credit: © Mark Wade


Titan 3A LargeTitan 3A Large
Credit: © Mark Wade



1964 September 1 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Titan. Launch Vehicle: Titan IIIA. FAILURE: Transtage pressurization failure caused premature shutdown.. Failed Stage: U.
1964 December 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Titan. Launch Vehicle: Titan IIIA.
1965 February 11 - . 15:19 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Titan. Launch Vehicle: Titan IIIA.
1965 May 6 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Titan. Launch Vehicle: Titan IIIA.

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