Accession Number : AD0852235

Title :   Factory Acceptance Testing of Missile 40E.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 01 SEP 1961

Pagination or Media Count : 65

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; Propellant utilization system; Propulsion system; Range safety command system; and Telemetry system.

Descriptors :   (*SURFACE TO SURFACE MISSILES, CHECKOUT PROCEDURES), ELECTRICAL EQUIPMENT, FLIGHT CONTROL SYSTEMS, INERTIAL GUIDANCE, 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