Accession Number:

AD0829233

Title:

PRELIMINARY TEST PROCEDURES FOR TESTING XSM-65A MISSILE PROPULSION SYSTEM INSTALLATION 7-20001.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

Report Date:

1956-04-30

Pagination or Media Count:

32.0

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