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

Authors: Louis Berman; NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA

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.

Limitations:

APPROVED FOR PUBLIC RELEASE

Pages:

Report Date:

25 MAR 74

Report Number:

A020623

Keywords relating to this report:

*FATIGUE TESTS(MECHANICS)

*FATIGUE TESTS_MECHANICS_

*JET TRANSPORT AIRCRAFT

LIFE EXPECTANCY_SERVICE LIFE_

LOAD DISTRIBUTION

STRUCTURAL INTEGRITY

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