Structural Scaling Parameters for Rectangular Flexible Blanket Solar Arrays
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Kirtland Air Force Base, New Mexico 87117
2. University of New Mexico, Albuquerque, New Mexico 87131
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32895
Reference24 articles.
1. MikulasM. M. “Structural Efficiency of Long Lightly Loaded Truss and Isogrid Columns for Space Applications,” NASA TM-78687, July 1978.
2. FelkelE.WolffG. “Flexible Rolled-Up Solar Array,” U.S. Air Force Aero Propulsion Lab., TR-72-61, Wright Patterson AFB, OH, June 1972.
3. Thermally induced bending vibrations of a flexible rolled-up solar array
4. Thermally induced vibrations of a self-shadowed split-blanket solar array
5. LindbergD. “A 928−m2 (10,000 ft2) Solar Array,” NASA TM-58106, Sept. 1972.
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