Accession Number : AD0854198
Title : Tactical Missile Launcher Feasibility Study. Book I.
Descriptive Note : Final rept.
Corporate Author : HONEYWELL INC HOPKINS MINN ORDNANCE DIV
Report Date : 1968
Pagination or Media Count : 132
Abstract : The document describes the development and the results of a study of the feasibility of designing a standard tactical missile launcher which is capable of carrying and launching hypothetical stores, weighing form 500 to 3,000 pounds, from the F100, F101, F104, and F105 aircraft. Store trajectories and flight clearances were investigated in a computer program. The results of the computer runs are analyzed and discussed. Structural and mechanical criteria have been established. (Author)
Descriptors : (*JET FIGHTERS, GUIDED MISSILE LAUNCHERS), (*GUIDED MISSILE LAUNCHERS, FEASIBILITY STUDIES), TACTICAL BOMBING, JET BOMBERS, AIR TO SURFACE MISSILES, GUIDED MISSILE TRAJECTORIES, AERODYNAMIC LOADING, AERODYNAMIC CHARACTERISTICS, EXTERNAL STORES, COMPUTER PROGRAMMING, MATHEMATICAL MODELS, EQUATIONS OF MOTION, NUMERICAL METHODS AND PROCEDURES, TABLES(DATA)
Subject Categories : Bombers
Attack and Fighter Aircraft
Air- and Space-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE