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A high strength, torsionally rigid, deployable and retractable mast for space applicationsA structural mast was developed which during and after full deployment produces a supporting structure with the characteristics of a high bending moment capability, high stiffness and, particularly important for instrument deployment, a high degree of position repeatability and torsional rigidity. These features were accomplished while providing and easily retractable mast with a high life cycle capability. Since these properties are consistent throughout the full range of deployed lengths, partial deployments or retractions can be utilized for checkout, balance, fine tuning or whatever other reason may be deemed necessary for operation modes or spacecraft stability.
Document ID
19830016621
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dibiasi, L.
(Fairchild Space and Electronics Co. Germantown, MD, United States)
Kramer, R.
(Fairchild Space and Electronics Co. Germantown, MD, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: JPL The 17th Aerospace Mech. Symp.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
83N24892
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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