'E' Launcher Tie Down Mechanism Functional Test.
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
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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
- Couplers, Fasteners and Joints
- Guided Missile Launching and Basing Support