Integral Rocket/Ramjet Propulsion System with Axial Admission Ports.

Abstract

The patent application relates to the design of a ramjet engine whereby air injection ports and fuel injection systems are arranged in a manner to enhance flame stability.

Document Details

Document Type
Technical Report
Publication Date
Jan 07, 1974
Accession Number
AD0164711

Entities

People

  • Edward T. Curran

Organizations

  • United States Department of the Air Force

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Engineering
  • Engines
  • Fuel Injection
  • Integrals
  • Mechanical Engineering
  • Patent Applications
  • Patents
  • Propulsion Systems
  • Ramjet Engines
  • Thermal Propulsion Systems

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.