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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.
Information on aircraft gives the type, and if available, the serial number of the operator in italics, the construction number (c/n), also known as the manufacturer's serial number, exterior codes in apostrophes, nicknames (if any) in quotation marks, flight call sign in italics, and operating units.
Cutaway of Space Shuttle external tank. Autogenous pressurization is the use of self-generated gaseous propellant to pressurize liquid propellant in rockets.Traditional liquid-propellant rockets have been most often pressurized with other gases, such as helium, which necessitates carrying the pressurant tanks along with the plumbing and control system to use it.
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.
The first aircraft carrier commissioned into the U.S. Navy was USS Langley (CV-1) on 20 March 1922. The Langley was a converted Proteus-class collier, originally commissioned as USS Jupiter (AC-3). [1]
Sometimes called a check valve or a backflow preventer, a chemigation valve is an apparatus designed to protect water supplies from agricultural chemicals used during chemigation, the application of chemicals such as fertilizers and pesticides through irrigation water. [1]
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