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Progress in the Phase 0 Model Development of a STAR Concept for Dynamics and Control TestingThe paper describes progress in the development of a lightweight, deployable passive Synthetic Thinned Aperture Radiometer (STAR). The spacecraft concept presented will enable the realization of 10 km resolution global soil moisture and ocean salinity measurements at 1.41 GHz. The focus of this work was on definition of an approximately 1/3-scaled, 5-meter Phase 0 test article for concept demonstration and dynamics and control testing. Design requirements, parameters and a multi-parameter, hybrid scaling approach for the dynamically scaled test model were established. The El Scaling Approach that was established allows designers freedom to define the cross section of scaled, lightweight structural components that is most convenient for manufacturing when the mass of the component is small compared to the overall system mass. Static and dynamic response analysis was conducted on analytical models to evaluate system level performance and to optimize panel geometry for optimal tension load distribution.
Document ID
20030112133
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Woods-Vedeler, Jessica A.
(NASA Langley Research Center Hampton, VA, United States)
Armand, Sasan C.
(Swales Aerospace Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2003
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2003-212645
NAS 1.15:212645
L-19002
Report Number: NASA/TM-2003-212645
Report Number: NAS 1.15:212645
Report Number: L-19002
Funding Number(s)
OTHER: 23-755-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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