FAST OPERATING VALVE FOR FEEDING A LIQUID, E.G., A FUEL COMPONENT INTO A LIQUID-PROPELLANT ROCKET ENGINE,

Abstract

The object of the invention is a rapid-action valve for the feeding of a liquid, for example, the fuel component into a liquid-propellant rocket engine, which contains a body, a membrane covering the passage section of the flow part, and a membrane-piercing organ with a pyroactuator. For the purpose of lessening the weight while preserving the dependability the 'piroprovod' (fire duct) is designed not connected in the power system with the body and separated from the flow part by a flexible diaphragm controlling the piercing organ and insulating the body from the highpressure gases. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 29, 1965
Accession Number
AD0620073

Entities

People

  • A. S. Ryzhkin
  • Tu. S. Tyurin
  • Yu. V. Belyaev
  • Z. D. Denisova

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Coverings
  • Energetic Materials
  • Engines
  • Inventions
  • Liquid Propellant Rocket Engines
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Membranes
  • Patents
  • Propellants
  • Rocket Engines
  • Rocket Propellants
  • Rockets
  • Skeletal Muscle

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Combustion and Flow Dynamics.
  • Electrical Engineering

Technology Areas

  • Microelectronics