The document contains inertial load tables and air load tables relative to 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 from 500 to 3,000 pounds, from the F100, F101, F104 and F105 aircraft.
Tactical Missile Launcher Feasibility Study. Book II
1968
241 pages
Report
No indication
English
Missile Technology , Aircraft , Jet fighters , Guided missile launchers , Feasibility studies , Tactical bombing , 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-101 aircraft , F-105 aircraft , F-104 aircraft
NTIS | 1970
NTIS | 1964
|NTIS | 1965
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