Accession Number : AD0373336
Title : MAIN TANK INJECTION FOR PACKAGED LIQUID MISSILES. VOLUME I. SYSTEMS ANALYSIS AND COMPONENT TEST.
Descriptive Note : Rept. for 24 Jan-20 May 66 on Phase 1,
Corporate Author : MARTIN CO DENVER COLO
Personal Author(s) : Howell ,J. Carney ; Fester ,Dale A. ; Balzer ,Daniel L. ; Bingham ,P. E. ; Dowell,D. W.
Report Date : JUN 1966
Pagination or Media Count : 186
Abstract : A study is being conducted on the use of main tank injection (MTI) for pressurization of packaged liquid missile propellant tanks. The propellants for this short-range, air-to-ground weapon system are MHF-5 fuel and Compound A oxidizer. This report presents the analytical evaluation of propellant orientation subsystems and MTI performance together with the results of limited tests on the compatibility of flexing components with hot Compound A. Analyses were conducted to define the vehicle propulsion system configuration and a program reference mission.
Descriptors : (*AIR TO SURFACE MISSILES, PROPELLANT TANKS), (*PROPELLANT TANKS, PRESSURIZATION), LIQUID PROPELLANT ROCKET ENGINES, INJECTION, PERFORMANCE(ENGINEERING) (U) CONFIGURATION, HYDRAZINE DERIVATIVES, PROPELLANT CONTROL, CAPILLARY TUBES, COMPATIBILITY, LIQUID ROCKET FUELS, LIQUID ROCKET OXIDIZERS, MECHANICAL PROPERTIES, PACKAGING, MISSION PROFILES, HYPERGOLIC IGNITION, ALCOHOLS, MATHEMATICAL MODELS, MATHEMATICAL PREDICTION, ENVIRONMENTAL TESTS, NICKEL ALLOYS, STAINLESS STEEL, SYSTEMS ENGINEERING, FLUID FILTERS, INJECTORS, FUEL INJECTION, PHYSICAL PROPERTIES
Subject Categories : Air- and Space-launched Guided Missiles
Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE