MAIN LANDING GEAR DROP TEST REPORT

Abstract

The shock absorber portion of the 1510L100 Main Landing Gear, but using a dummy cylinder, was tested on 2 August 1963, in accordance with the H. W. Loud Test Procedure 1510LTP-4, Revision 'A'. The report presents the successful completion of the established test requirements.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1964
Accession Number
AD0646282

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Pressure
  • Aircrafts
  • Army Aviation
  • California
  • Department Of Defense
  • Drop Tests
  • Drops
  • Export Controls
  • Governments
  • Landing Gear
  • Lift Fans
  • Procurement
  • Research Aircraft
  • Shock Absorbers
  • United States
  • United States Government
  • Virginia

Readers

  • Aerospace Engineering
  • Explosive Engineering.
  • Systems Analysis and Design