The purpose of this study was to develop a computer program by which to optimize the various missile parameters available to the missile designer of a short range (one to ten mile radius) missile. The missile model used in this study was required to have the capability of intercepting a target with an unspecified heading at an initial range of three miles, and an angle-off-boresight of 45 deg. The missile intercepts the target by flying a hard-over turn initially, followed by a straight-line trajectory until impact. This study demonstrates the feasibility of using a computer model, similar to the one in this paper, to check out the capabilities claimed by contractors for their missile designs.
Method for Aerodynamic and Propulsion Design Optimization of the Short Range Dogfight Missile
1972
23 pages
Report
Keine Angabe
Englisch
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