Accession Number : AD0842592

Title :   'E' Launcher Tie Down Mechanism Functional Test.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Smirin, J. M.

Report Date : 14 NOV 1960

Pagination or Media Count : 14

Abstract : The objective of the test was to perform a functional test on the 'E' horizontal launcher tie down installation (27-49660) to substantiate their structural capabilities and to determine adjustment procedures required on the mechanism to make it operable. (Author)

Descriptors :   (*GUIDED MISSILE LAUNCHERS, RELEASE MECHANISMS), (*RELEASE MECHANISMS, STRUCTURAL PROPERTIES), INSTALLATION, SEQUENCES(MATHEMATICS), POSITIONING DEVICES(MACHINERY), INSTRUCTION MANUALS, STRAIN GAGES, DEFLECTION, SURFACE TO SURFACE MISSILES.

Subject Categories : Couplers, Fasteners, and Joints
      Guided Missile Launching and Basing Support
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE