Reverse Flow Aft Inlet Ramjet System

Abstract

The patent application relates generally to integral rocket/ramjets and, in particular, to ramjets having multiple, aft-mounted air inlets and used to propel missiles.

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Document Details

Document Type
Technical Report
Publication Date
Mar 11, 1975
Accession Number
ADD000689

Entities

People

  • Edward T. Curran

Organizations

  • United States Department of the Air Force

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Launched
  • Aircrafts
  • Burning Rate
  • Chambers
  • Combustion
  • Combustion Chambers
  • Engines
  • Exhaust Nozzles
  • Flow
  • Fuels
  • Injectors
  • Inventions
  • Propulsion Systems
  • Ramjet Engines
  • Rocket Engines
  • Secondary Flow

Fields of Study

  • Physics