NASA NTRS · 20040171171
Design for a Unitary Graphite Composite Instrument Boom
Abstract
This 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.
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Alexander, Wes, Carlos, Rene, Sturm, James, Rossoni, Peter. 2004-01-01. Design for a Unitary Graphite Composite Instrument Boom. https://ntrs.nasa.gov/citations/20040171171
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