NOSE LANDING GEAR DROP TEST REPORT

Abstract

The results of the tests demonstrate satisfactory energy absorbtion characteristics of the shock absorber. The first test condition results meets the requirements of the deviation allowance. The vertical reaction exceeds the original requirements for approximately .05 seconds at a strut stroke of 4.15 inches with a maximum of 6600 pounds. The second condition results meets the test requirements. The official test for condition three was run with an additional 200 pounds on the jig that was anticipated to correct for friction in the drop tower. The results indicate, however, excessive energy input. A prior run is also included with the correct jig weight and with insufficient energy input to show the effect of the weight change. Both runs are well within the maximum allowable vertical reaction.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1965
Accession Number
AD0645999

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

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

Readers

  • Computational Modeling and Simulation
  • Explosive Engineering.
  • Materials Science