DEVICE FOR CUTOFF OF FUEL SUPPLY TO A LIQUID-PROPELLANT ROCKET ENGINE,

Abstract

A device for cutting off the supply of fuel to a liquidpropellant rocket engine is described. The valve consist of a body (housing) inside of which there are conical seats and there is placed a valve controllable by a pyromechanism. The plate and stock are provided with conical sealing bands. The sealing bands have the distinguishing feature of creating a more dependable hermetic sealing through the assuring of independent wedging of the sealing bands. The stock of the valve is designed from two parts mutually movable in the axial direction, joined to each other by a sleeve. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 23, 1965
Accession Number
AD0619469

Entities

People

  • A. Yu. Polinovskii
  • I. M. Nosotsov
  • L. A. Arinushkin

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Energetic Materials
  • Engines
  • Liquid Propellant Rocket Engines
  • Liquid Propellants
  • Propellants
  • Rocket Engines
  • Rocket Propellants
  • Rockets

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Rocket Propulsion.