Accession Number : AD0829233
Title : PRELIMINARY TEST PROCEDURES FOR TESTING XSM-65A MISSILE PROPULSION SYSTEM INSTALLATION 7-20001.
Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV
Report Date : 30 APR 1956
Pagination or Media Count : 32
Abstract : This Test Procedure provides test equipment operating instructions required to perform post-installation operational acceptance tests of the Missile propulsion system. The test procedure is divided into two parts: (1) Integrated component operation test, (2) Propulsion system sequence operation test. Part 1 must be successfully completed before beginning Part 2, and the checkout operations must follow in the order given in this procedure. (Author)
Descriptors : (*SURFACE TO SURFACE MISSILES, LIQUID PROPELLANT ROCKET ENGINES), (*LIQUID PROPELLANT ROCKET ENGINES, TEST METHODS), VALVES, PUMPS, CHECKOUT EQUIPMENT, CHECKOUT PROCEDURES, PRESSURE, GAS GENERATING SYSTEMS, INSTRUCTION MANUALS, MILITARY REQUIREMENTS, ACCEPTABILITY, TEST EQUIPMENT, SPECIFICATIONS.
Subject Categories : Surface-launched Guided Missiles
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE