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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.
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Pages in category "Titan (rocket family)" ... Titan IV; Transtage This page was last edited on 24 January 2019, at 23:10 (UTC). Text is available ...
The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.
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 ...
This page is an incomplete list of orbital rocket engine data and specifications. ... Black Arrow: 2nd RP-1 / H 2 O 2 ... Titan IV: Booster: PBAN: Solid fuel 272 [101 ...
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