The concept of pulsed rocket velocity control is defined as well as its integration with a total missile system. The research, development and testing are summarized. Test results, conclusions and recommendations are included. A Pulsed Rocket Velocity Control System was breadboarded and tested. Twenty-three static tests were made to evaluate the pulsed mode of operation. Computer flight simulations were made to determine operational characteristics and the effects of experimentally determined time delays. (Author)


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