4.3 Article

Thermal Design and Analysis of Unfurlable CFRP Skin-Based Parabolic Reflector for Spaceborne SAR Antenna

出版社

SPRINGER
DOI: 10.1007/s42405-020-00301-7

关键词

Synthetic aperture radar (SAR) antenna; Thermal distortion; Thermal design; On-orbit thermal environment; Carbon fiber reinforced plastic

资金

  1. Deployable SAR Reflector for Satellite Development Program (2019)
  2. Defense Acquisition Program Administration
  3. Agency for Defense Development

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This study focuses on the preliminary thermal design and analysis of a carbon fiber reinforced plastic skin-based unfurlable parabolic reflector for spaceborne SAR antennas. It highlights the importance of passive thermal designs with different coatings to minimize thermal distortion and gradient for optimal SAR performance. Additionally, the impact of solar panels on the reflector's thermal gradient is also investigated to further enhance antenna gain and SAR performance.
To ensure high-resolution image acquisition for a spaceborne parabolic synthetic aperture radar (SAR) antenna, an appropriate thermal design is important to minimize the thermal distortion of the antenna reflector in severe on-orbit thermal environments. This paper describes the results of a preliminary thermal design and the analysis of a carbon fiber reinforced plastic skin-based unfurlable parabolic reflector for use in a spaceborne SAR antenna. The effectiveness of passive thermal designs for an antenna reflector using different thermal coatings was investigated with on-orbit thermal analyses according to the various antenna look angles to derive the most suitable design for minimizing the thermal gradient of the reflector. This contributes to minimize loss in antenna gain to ensure the SAR performance. In addition, the influence of the solar panel on the thermal gradient of the reflector was also analyzed because it is also important in affecting the thermal distortion.

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