Damping Behavior of Dehavilland Stem Booms
Author: R. E. Predmore
Publisher:
Published: 1967
Total Pages: 20
ISBN-13:
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Author: R. E. Predmore
Publisher:
Published: 1967
Total Pages: 20
ISBN-13:
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Author: Goddard Space Flight Center
Publisher:
Published: 1967
Total Pages: 168
ISBN-13:
DOWNLOAD EBOOKIncludes lists of GSFC technical documents published internally, not widely distributed, and: NASA technical memorandums, technical notes, and technical reports.
Author:
Publisher:
Published: 1967
Total Pages:
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DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1966
Total Pages: 1320
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1970
Total Pages: 1348
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DOWNLOAD EBOOKAuthor: C. L. Staugaitis
Publisher:
Published: 1970
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKThe mechanical (static and dynamic) behavior of a number of boom designs applicable to gravity gradient and antenna use were investigated. Bending stiffness, critical bending moment, damping, and transverse (fundamental bending) frequency were the principal properties measured. The structural integrity of two boom designs was also evaluated when subjected to cyclic loading conditions. The results are analyzed in terms of structural performance and conformance to elastic behavior as predicted by theory for thin-walled tubes.
Author: Harold P. Frisch
Publisher:
Published: 1970
Total Pages: 124
ISBN-13:
DOWNLOAD EBOOKLong thin-walled cylinders of open section (STEM type booms) have been used on many satellites either for experimentation or Gravity Gradient stabilization. Equations for the coupled transverse plus torsional oscillations of a long open section cylinder in direct sunlight are derived. Numerical results show that unstable thermally induced oscillations can be excited solely by the impinging thermal energy of the sun. It is shown that this is a direct result of the boom's extreme weakness in torsion. By literally zippering the boom's open section, to increase its torsional rigidity, the problem can be eliminated. Flight data from OGO IV, V, VI and RAE are cited to support the theoretical findings.