Accession Number:

AD0852249

Title:

Factory Acceptance Testing of Missile 22F.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-09-26

Pagination or Media Count:

33.0

Abstract:

Before conducting the missile composite checkout, successful performance of each individual system installed on the missile must be determined. The following is a list of the procedures used for acceptance testing of each system Electrical system Flight control system Inertial guidance system Propellant utilization system Propulsion system. Author

Descriptors:

• (*SURFACE TO SURFACE MISSILES
• CHECKOUT PROCEDURES)
• ELECTRICAL EQUIPMENT
• FLIGHT CONTROL SYSTEMS
• INERTIAL NAVIGATION
• LIQUID ROCKET PROPELLANTS
• LIQUID PROPELLANT ROCKET ENGINES

Subject Categories:

• Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE