Development of a Three-Stage Supersonic Hot Gas Reaction Valve,

Abstract

The purpose of the report is to describe briefly the performance of a three-stage, fluidic, hot gas, jet reaction control valve developed for the MARS flight control system. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 17, 1968
Accession Number
AD0872090

Entities

People

  • J. Dunaway
  • V. Ayre

Tags

DTIC Thesaurus Topics

  • Control Systems
  • Flight Control Systems
  • Gases
  • Hot Gases

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Robotics and Automation.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow