Titan 3M (original) (raw)


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Titan 3M


Part of Titan


Titan 3M
Titan 3M
Credit: © Mark Wade

American orbital launch vehicle. Man-rated launch vehicle designed for MOL and other missions of the 1970's. Malfunction Detection System initiated abort procedures during launch. Also suited for launch of 'bulbous and lifting body payloads'. 7 segment UA1207 motors developed but not used until Titan 4 in 1990's. Cancelled with MOL program in 1969.

Status: Development ended 1967. Payload: 17,000 kg (37,000 lb). Thrust: 12,821.00 kN (2,882,275 lbf). Gross mass: 836,560 kg (1,844,290 lb). Height: 39.00 m (127.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 17,000 kg (37,000 lb) to a 185 km orbit. Launch Price $: 22.000 million in 1965 dollars.

Stage Data - Titan 3M



Family: orbital launch vehicle. Country: USA. Engines: LR87-11, LR91-11. Spacecraft: Gemini Ferry, MOL. Launch Sites: Vandenberg. Stages: Titan 3B-1, Titan 3B-2, UA1207. Agency: Martin.



1965 August 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg. LV Family: Titan. Launch Vehicle: Titan 3M.


1969 April 27 - . LV Family: Titan. Launch Vehicle: Titan 3M.


1970 Late - . LV Family: Titan. Launch Vehicle: Titan 3M.


1971 - . LV Family: Titan. Launch Vehicle: Titan 3M.


1972 Early - . LV Family: Titan. Launch Vehicle: Titan 3M.


1972 Late - . LV Family: Titan. Launch Vehicle: Titan 3M.


1973 - . LV Family: Titan. Launch Vehicle: Titan 3M.


1974 - . LV Family: Titan. Launch Vehicle: Titan 3M.


1975 - . LV Family: Titan. Launch Vehicle: Titan 3M.



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