A simplified preliminary design capability for erectable precision segmented reflectors is presented. This design capability permits a rapid assessment of a wide range of reflector parameters as well as new structural concepts and materials. The preliminary design approach was applied to a range of precision reflectors from 10 meters to 100 meters in diameter while considering standard design drivers. The design drivers considered were: weight, fundamental frequency, launch packaging volume, part count, and on-orbit assembly time. For the range of parameters considered, on-orbit assembly time was identified as the major design driver. A family of modular panels is introduced which can significantly reduce the number of reflector parts and the on-orbit assembly time.
Preliminary design considerations for 10 to 40 meter-diameter precision truss reflectors
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference ; 1990 ; Long Beach, CA, United States
01.01.1990
Aufsatz (Konferenz)
Keine Angabe
Englisch
Thermal Distortion of Over 10 Meter Diameter Reflectors Formed by Truss Structure
British Library Conference Proceedings | 1997
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