PRELIMINARY TEST PROCEDURES FOR TESTING XSM-65A MISSILE PROPULSION SYSTEM INSTALLATION 7-20001.
GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV
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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
- Surface-Launched Guided Missiles
- Liquid Propellant Rocket Engines