EFFECT OF FIRING ROCKET SHELLS ON THE PERFORMANCE OF TURBOJET POWER PLANT,

Abstract

The effects of firing rocket ammunition on the performance of axial flow turbojet engines are considered. The causes and effects of rocket launchings from airborne aircraft are discussed. Several recommendations for the prevention of these problems are given. The dynamic, thermal, and chemical effects on the performance of the power plant are described.

Document Details

Document Type
Technical Report
Publication Date
Nov 12, 1964
Accession Number
AD0608451

Entities

People

  • J. Szymankiewicz

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Airborne
  • Aircrafts
  • Ammunition
  • Axial Flow
  • Engines
  • Flow
  • Jet Aircraft
  • Launching
  • Rocket Launching
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • ballistics.