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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.
The SRMU is a three-segment solid rocket motor. Each segment has a casing wound from graphite fibre composite and an insulation system of EPDM rubber and kevlar. [1] The casing is filled with a fuel grain composed primarily of ammonium perchlorate and aluminium, joined by a HTPB binder. [2]
Final flight of Titan IIIC 11 May 18:45 Titan III(23)D: 23D-24 VAFB SLC-4E: LEO: Success OPS-5642 SSF-D-4: 30 October 04:05 Titan 34D/IUS: 4D-5 34D-1 CCAFS LC-40: GSO: Success OPS-9446 OPS-6451 DSCS III-A1: First flight of Titan 34D 17 November 21:22 Titan III(23)D: 23D-23 VAFB SLC-4E: LEO: Success OPS-9627 Final flight of Titan IIID
The Titan II also used storable propellants: Aerozine 50 fuel, which is a 1:1 mixture of hydrazine and unsymmetrical dimethylhydrazine (UDMH), and dinitrogen tetroxide oxidizer. The Titan I, whose liquid oxygen oxidizer had to be loaded immediately before launching, had to be raised from its silo and fueled before launch.
An engineering drawing is a type of technical drawing that is used to convey information about an object. A common use is to specify the geometry necessary for the construction of a component and is called a detail drawing. Usually, a number of drawings are necessary to completely specify even a simple component.
An exploded-view drawing is a diagram, picture, schematic or technical drawing of an object, that shows the relationship or order of assembly of various parts. [ 1 ] It shows the components of an object slightly separated by distance, or suspended in surrounding space in the case of a three- dimensional exploded diagram.
Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005. [4] Launches were conducted from Cape Canaveral Air Force Station, Florida [5] and Vandenberg Air Force Base, California.
In the process industry, a standard set of symbols is used to prepare drawings of processes. The instrument symbols used in these drawings are generally based on International Society of Automation (ISA) Standard S5.1; The primary schematic drawing used for laying out a process control installation. They usually contain the following information: