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

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

Active / Technical Report | Accession Number: AD0829233 |

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

Author(s):

No Author(s) Identified

Author Organization(s):

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Pagination:

0032

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

GDC-Z17005(20)

Subject Terms

Joint Capability Areas:

JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means

Communities of Interest:

Weapons Technologies

Descriptor(s):

(*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

Field(s)/Group(s):

Surface-Launched Guided Missiles, Liquid Propellant Rocket Engines

Keyword(s):

ATLAS, XSM 65B MISSILES

Report Date:

1956 Apr 30