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Design for a Unitary Graphite Composite Instrument BoomThis paper describes development of a Unitary graphite composite instrument boom that incorporates carpenter-tape like hinges for stowage. While light and stiff, graphite composite is not ordinarily thought of as a flexible material. This design has taken advantage of the stiffness of the composite in tubular geometry, yet leveraged its thin- section behavior to place flexibility at the required locations. Key is the proprietary layup, which results in a tough yet flexible hinge capable of rotating over 90 degrees in each direction. When the boom deploys, there is enough torque to overcome parasitic resistance from harness, etc. It will snap to the fully extended, rigid shape. The design has addressed materials issues such as out-of-plane bending, edge cracking, and interlaminar ply separation.
Document ID
20040171171
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Alexander, Wes
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Carlos, Rene
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Sturm, James
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Rossoni, Peter
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Meeting Information
Meeting: 2004 National Space and Missile Materials Symposium
Location: Seattle, WA
Country: United States
Start Date: June 21, 2004
End Date: June 25, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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