THE DEVELOPMENT OF A HOT GAS REACTION CONTROL VALVE FOR AN ANTITANK MISSILE,

Abstract

The objective of this program was to design and develop a hot gas jet reaction control valve capable of operating at 100 cps or greater, with an output force of 4.5 pounds. It was also required that the valve be compatible with the existing electronic driving circuit having a pulse width modulated output. The jet reaction control valve developed in this program was capable of valving 2100 F gas. The maximum switching frequency of the valve was 150 cps over a supply pressure range of 800 to 1400 psi. The 150 cps operating frequency achieved with this valve was considered to be approaching the maximum practical frequency for an electromechanically driven, single stage valve of this force level. Since the valve was designed to operate on atmospheric pressure, control flow was limited by the control passage width and the pressure of the expanded power jet in the mixing region. Restrictions on the valve envelope size would not permit either of these parameters to be increased. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 15, 1965
Accession Number
AD0478067

Entities

People

  • J. C. Dunaway

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Anti-Tank Missiles
  • Barometric Pressure
  • Frequency
  • Gases
  • Hot Gases
  • Switching

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • Internal Combustion Engine (ICE) Technology.

Technology Areas

  • Microelectronics