Accession Number:

AD0842592

Title:

'E' Launcher Tie Down Mechanism Functional Test.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

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

Subject Categories:

  • Couplers, Fasteners and Joints
  • Guided Missile Launching and Basing Support
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE