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