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The Titan IIIE or Titan 3E, also known as the Titan III-Centaur, was an American expendable launch system. Launched seven times between 1974 and 1977, [ 4 ] it enabled several high-profile NASA missions, including the Voyager and Viking planetary probes and the joint West Germany-U.S. Helios spacecraft .
First crewed Titan launch 25 March 02:15 Titan II: B-60 VAFB LC-395-B: Suborbital: ... First flight of Titan IIIE. Centaur LOX turbopump malfunction. RSO T+525 seconds.
A Titan IIIE-Centaur rocket (Centaur D-1T stage) launches Voyager 2. The Centaur D-1T (powered by RL10A-3-3 engines) was an improved version for use on the far more powerful Titan III booster in the 1970s, [47] with the first launch of the resulting Titan IIIE in 1974. The Titan IIIE more than tripled the payload capacity of Atlas-Centaur, and ...
Titan IIIE Centaur-D1T [8] NASA: Flyby Successful Closest approach on 12 November 1980 at 23:45 UTC. Flew past Titan, Tethys, Mimas, Enceladus and Rhea. [10] [9] 4 Cassini–Huygens: Cassini: 15 October 1997 [2] Titan IV(401)B Centaur-T [18] NASA: Orbiter Successful Huygens: ESA: Titan lander Successful Entered orbit 1 July 2004. First probe to ...
This comparison of retired orbital launch systems lists the attributes of all retired individual rocket configurations designed to reach orbit. For a list of proposed rocket configurations or individual configurations currently being launched check out Comparison of Orbital Launch Systems .
The Titan IVB was the last Titan rocket to remain in service, making its penultimate launch from Cape Canaveral on 30 April 2005, followed by its final launch from Vandenberg Air Force Base on 19 October 2005, carrying the USA-186 optical imaging satellite for the National Reconnaissance Office.
Rocket Flight number Launch site LSP; Payload (⚀ = CubeSat) Operator Orbit Function Decay (UTC) Outcome Remarks 19 February 05:15 M-3H: Kagoshima Space Center LP-M ISAS: MS-T3 (Tansei 3) ISAS Highly elliptical orbit: Technology test: In orbit: Successful First flight of M-3H 16 June 10:51:00 Delta 2914: Cape Canaveral LC-17B: GOES 2: NOAA ...
Transtage was developed in anticipation of a requirement to launch military payloads to geostationary orbit; a contract for development of the stage was issued on 20 August 1962. [2] Transtage used a pressure-fed two-chamber configuration, using Aerozine 50 fuel and nitrogen tetroxide as oxidizer ; the thrust chambers were gimbaled for steering ...