Accession Number:

AD0842592

Title:

'E' Launcher Tie Down Mechanism Functional Test.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Smirin, J. M.

Report Date:

1960-11-14

Pagination or Media Count:

14.0

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