Accession Number : AD0784365

Title :   Preliminary Results Concerning the Improvements Realizable Through the Use of Variable Thrust Together with Engine Gimbaling for a Particular Interceptor Missile.

Descriptive Note : Technical rept.,


Personal Author(s) : Russak,I. Bert

Report Date : JUN 1974

Pagination or Media Count : 28

Abstract : Some interceptor missiles as presently formulated possess a programmed thrust magnitude history with a gimbaled engine to provide steering. One such missile was examined to determine whether performance can be improved if we allow a variable thrust magnitude together with engine gimbaling to provide control. Two trajectory optimization programs were written to provide an initial answer to this problem. Preliminary results indicate reductions in the time to intercept by as much as thirty per-cent over that obtained by the presently used guidance scheme. With tuning of the programs it seems reasonable to expect even greater improvements. (Author)

Descriptors :   *Guided missile countermeasures, *Interception probabilities, *Flight control systems, Antimissile defense systems, Intercept trajectories, Optimization, Mathematical models, Gimbals, Thrust control

Subject Categories : Antimissile Defense Systems
      Guided Missile Traj, Accuracy and Ballistics

Distribution Statement : APPROVED FOR PUBLIC RELEASE