Program Plan for Investigation of Model E-1/C-1 Airplane Catapult and Hold-Back Operations Capacity,

Abstract

A laboratory fatigue test will be performed on an E-1 airframe to determine whether the airframe will sustain the effects of 3,000 catapult launches without structural failure.

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Document Details

Document Type
Technical Report
Publication Date
Mar 25, 1974
Accession Number
ADA326020

Entities

People

  • Louis Berman

Organizations

  • Naval Air Warfare Center Warminster

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Airplanes
  • Classification
  • Engineering
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Fuselages
  • Landing Gear
  • Security
  • Ships
  • Simulations
  • Spars
  • Test Methods
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering