Accession Number : AD0852236

Title :   Factory Acceptance Testing of Missile 8F.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 09 SEP 1961

Pagination or Media Count : 84

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: Atlas optical beacon system; Azusa system; Electrical system; Flight control system; Inertial guidance system; Instrumentation beacon system; Propellant utilization system; Propulsion system; Range safety command system; and Telemetry system. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, CHECKOUT PROCEDURES), BEACONS, GUIDED MISSILE TRACKING SYSTEMS, ELECTRICAL EQUIPMENT, FLIGHT CONTROL SYSTEMS, INERTIAL NAVIGATION, LIQUID ROCKET PROPELLANTS, LIQUID PROPELLANT ROCKET ENGINES, GUIDED MISSILE SAFETY, TELEMETER SYSTEMS.

Subject Categories : Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE