Accession Number:

AD0852255

Title:

Factory Acceptance Testing of Missile 10F.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-10-02

Pagination or Media Count:

72.0

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 Azusa system Electrical system Flight control system Inertial guidance system Instrumentation beacon system Acoustica propellant utilization system Propulsion system, Range safety command system and Telemetry system. Author

Descriptors:

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

Subject Categories:

• Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE