Accession Number:

AD0852190

Title:

Factory Acceptance Testing of Missile 119D.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-11-08

Pagination or Media Count:

65.0

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 Guidance system Instrumentation range safety system Propellant utilization system and Propulsion system. Author

Descriptors:

• (*SURFACE TO SURFACE MISSILES
• CHECKOUT PROCEDURES)
• ELECTRICAL EQUIPMENT
• FLIGHT CONTROL SYSTEMS
• RADIO BEACONS
• GUIDED MISSILE SAFETY
• LIQUID ROCKET PROPELLANTS
• LIQUID PROPELLANT ROCKET ENGINES

Subject Categories:

• Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE