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Pages in category "Titan (rocket family)" The following 17 pages are in this category, out of 17 total. ... Code of Conduct; Developers; Statistics; Cookie statement;
Launch of a Titan 34D with two UA1206 boosters. UA120 was a family of American solid rocket boosters, manufactured by the Chemical Systems Division of United Aircraft (later United Technologies Corporation). [1] They were used as strap-on boosters for the Titan rocket family. [2] Several variants existed, with a varying number of segments.
Most of the Titan rockets were the Titan II ICBM and their civilian derivatives for NASA.The Titan II used the LR-87-5 engine, a modified version of the LR-87, that used a hypergolic propellant combination of nitrogen tetroxide (NTO) for its oxidizer and Aerozine 50 (a 50/50 mix of hydrazine and unsymmetrical dimethylhydrazine (UDMH) instead of the liquid oxygen and RP-1 propellant of the Titan I.
First flight of Titan 33B 22 April 15:30 Titan III(23)B: 23B-9 3B-31 VAFB SLC-4W: LEO: Success OPS-7899 Final flight of Titan 23B 5 May 07:43 Titan III(23)C: 23C-2 3C-20 CCAFS LC-40: GSO: Success OPS-3811 15 June 18:41 Titan III(23)D: 23D-1 VAFB SLC-4E: LEO: Success OPS-8709 First flight of Titan IIID 20 June 22:45 Titan II: B-12 VAFB LC-395-C ...
Titan II rocket launch with Clementine spacecraft (25 January 1994) Titan-II 23G-9 B-107 carrying DMSP-5D3 F-16 Final Titan II launch 18 Oct 2003 The first flight of the Titan II was in March 1962 and the missile, now designated LGM-25C, reached initial operating capability in October 1963.
The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American medium-lift launch vehicle derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta , into which the Glenn L. Martin Company , which built the original Titan II, had merged.
Download QR code; Print/export Download as PDF; Printable version; In other projects ... Titan (rocket family) (1 C, 19 P) U. Universal Rocket (rocket family) (2 C ...
Used on the Titan I, the LR87-3 burned liquid oxygen and RP-1. [4] Following the retirement of the Titan missile program, these engines saw no further use. [citation needed] The LR87-3 was also operated with NTO/Aerozine 50 and ground tested with LOX/H2 (with a new fuel pump), making it one of very few engines to have been run on three different propellant combinations.