Analysis and ground testing for validation of the Inflatable Sunshield In Space (ISIS) experiment
Author:
Affiliation:
1. USRA, Greenbelt, MD
2. NASA, Goddard Space Flight Center, Greenbelt, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1638
Reference10 articles.
1. The nodal concept of deployment and the scale model testing of its application to a membrane antenna
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1. Structural Analysis and Testing of a 1/20th Scale NGST Sunshield Membrane Layer;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07
2. Finite Element Analysis of Wrinkled Membrane Stuctures for Sunshield Applications;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22
3. Modeling and analysis of structural dynamics for a one-tenth scale model NGST sunshield;19th AIAA Applied Aerodynamics Conference;2001-06-11
4. Thin film membrane wrinkling due to mechanical and thermal loads;19th AIAA Applied Aerodynamics Conference;2001-06-11
5. Dynamic testing of a subscale sunshield for the Next Generation Space Telescope (NGST);19th AIAA Applied Aerodynamics Conference;2001-06-11
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