PERFORMANCE TEST UNDER LABORATORY CONDITIONS OF LAU-25/A(XN-1) FLARE LAUNCHER EJECTION SYSTEM

Abstract

The performance test of the LAU-25/A(XN-1) flare launcher ejection and retention mechanism has been successfully completed with all components functioning satisfactorily. The test was made to demonstrate that all of the components of the ejection mechanism would function properly prior to incorporation into the final design. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1961
Accession Number
AD0270498

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Buildings And Structures
  • Ejection
  • Launchers
  • Performance Tests

Readers

  • Aviation Science / Aeronautics.
  • ballistics.