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A clamp mechanism for deployable three-ton payloadsThe requirements, capabilities, and unique design features of the instrument payload subsystem payload clamp assembly (PCA) are presented. The PCA is designed to have the flexibility to accommodate a wide payload range varying from 0.5 m to 3 m in diameter and from 500 kg to 3000 kg mass. This is achieved by modular clamp design in connection with replaceable struts. The design features include clamping of payload in a statically determined way and actuation of clamp latches by means of single linear actuator via ropes. The vibration and TV environmental conditions for the mechanism are extremely severe. A structural and prototype model was built. Test results of the operating characteristic are presented. In addition, problems of tribology are highlighted.
Document ID
19810013882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Birner, R.
(Messerschmitt-Boelkow-Blohm G.m.b.H. Munich, Germany)
Ral, H.
(Messerschmitt-Boelkow-Blohm G.m.b.H. Munich, Germany)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Publication Information
Publication: NASA. Marshall Space Flight Center The 15th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
81N22413
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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