PULSED ROCKET VELOCITY CONTROL FINAL PROGRAM REPORT

Abstract

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)

Document Details

Document Type
Technical Report
Publication Date
Aug 10, 1964
Accession Number
AD0353781

Entities

People

  • J. S. Gates
  • P. Varhola
  • T. F. Runyan
  • T. Sullivan

Organizations

  • Stellantis North America (formerly Chrysler)

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Computer Simulations
  • Computers
  • Control Simulators
  • Control Systems
  • Education
  • Flight Simulations
  • Flight Simulators
  • Simulations
  • Simulators
  • Static Tests
  • Synthetic Environment Simulations
  • Teaching Methods
  • Training
  • Training Devices

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Fluid Dynamics.
  • Systems Analysis and Design