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)
Tactical Missile Launcher Feasibility Study. Book I
1968
132 pages
Report
Keine Angabe
Englisch
Missile Technology , Aircraft , Jet fighters , 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) , Bullpup missiles , F-100 aircraft , F-105 aircraft , F-101 aircraft , F-104 aircraft
NTIS | 1970
NTIS | 1964
|NTIS | 1965
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