High Impact Shock Test of a General Electric LM2500 Propulsion Gas Turbine Module

This paper discusses the high impact shock testing of a General Electric Propulsion Gas Turbine Module to the requirements of Military Specification MIL-S-901C. This shock qualification is just one of a comprehensive program of tests to be, performed to fully qualify the LM2500 Gas Turbine and the DD-963 Propulsion System components specifically for the Spruance (DD-963) Class Destroyers. The description of the gas turbine and the preparation for, and the conduct of the shock test, and a review of the shock test results are presented.