Accession Number : AD0842731
Title : IOC-2 Hold Down and Release System Confidence Test.
Descriptive Note : Final rept.,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Cawood, Carl V.
Report Date : 27 JUN 1960
Pagination or Media Count : 91
Abstract : Testing was conducted under simulated operational and environmental temperature conditions to ensure proper system operation and to prove component-system compatibility of the hold down and release system of the Atlas missile launcher.
Descriptors : *RELEASE MECHANISMS), (*GUIDED MISSILE LAUNCHERS, RELIABILITY, OPERATION, SEQUENCES(MATHEMATICS), HYDRAULIC EQUIPMENT, TRANSDUCERS, VALVES, CONTROL SYSTEMS, PUMPS, ENVIRONMENTAL TESTS, SURFACE TO SURFACE MISSILES.
Subject Categories : Couplers, Fasteners, and Joints
Guided Missile Launching and Basing Support
Surface-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE