Accession Number : ADA326020

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

Corporate Author : NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA

Personal Author(s) : Berman, Louis

PDF Url : ADA326020

Report Date : 25 MAR 1974

Pagination or Media Count : 31

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.

Descriptors :   *JET TRANSPORT AIRCRAFT, *FATIGUE TESTS(MECHANICS), *SHIP LAUNCHED, LOAD DISTRIBUTION, LIFE EXPECTANCY(SERVICE LIFE), FUSELAGES, TAKEOFF, CATAPULTS, FAILURE(MECHANICS), FLIGHT LOADS, LAUNCHING SITES, STRUCTURAL INTEGRITY.

Subject Categories : Transport Aircraft
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE