Accession Number : AD0852255

Title :   Factory Acceptance Testing of Missile 10F.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 02 OCT 1961

Pagination or Media Count : 72

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