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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.
Part of the Titan rocket family, the Titan II ICBM was the successor to the Titan I, with double the payload. Unlike the Titan I, it used hydrazine -based hypergolic propellant which was storable and reliably ignited.
Titan II: N-32 CCAFS LC-15: Suborbital: Success 13 March Titan II: N-30 VAFB LC-395-C: Suborbital: Success 24 March 01:42 Titan II: N-33 CCAFS LC-15: Suborbital: Success Pod T-207: Gemini Malfunction Detection System test 6 April 16:00:01 Titan II GLV: GT-1 CCAFS LC-19: LEO: Success Gemini 1: First Gemini launch, first orbital Titan launch 9 ...
The Titan II was a two-stage liquid-fuel rocket, using a hypergolic propellant combination of Aerozine 50 fuel and nitrogen tetroxide oxidizer. The first stage was powered by an LR87 engine (with two combustion chambers and nozzles, fed by separate sets of turbomachinery), [ 2 ] [ 3 ] and the second stage was propelled by an LR-91 engine.
Pages in category "Titan (rocket family)" The following 17 pages are in this category, out of 17 total. ... LGM-25C Titan II; List of Titan launches; T. Titan 23G ...
A fourteenth rocket, G-10, based on Titan II B-108, but incorporating an oxygen tank from B-80, was not launched and is preserved at the Evergreen Aviation & Space Museum in McMinnville, Oregon. The remaining 42 Titan II missiles were stored at Davis-Monthan AFB with most being broken up for salvage. Four were transferred to museums.
The Titan III family consisted of an enhanced Titan II core with or without solid rocket strap-on boosters and an assortment of upper stages. All Solid Rocket Motor (SRM)-equipped Titans (IIIC, IIID, IIIE, 34D, and IV) launched with only the SRMs firing at liftoff, the core stage not activating until T+105 seconds, shortly before SRM jettison.
The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena (which had a smaller diameter than the Titan) enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The ...