BEACON eSpace at Jet Propulsion Laboratory >
JPL Technical Report Server >
JPL TRS 1992+ >
Please use this identifier to cite or link to this item:
|Title: ||A dual-polarized, dual-frequency, corrugated feed horn for SMAP|
|Authors: ||Focardi, Paolo|
Brown, Paula R.
|Keywords: ||Horn antennas|
|Issue Date: ||8-Jul-2012 |
|Publisher: ||Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012.|
|Citation: ||IEEE International Symposium on Antennas and Propagation, Chicago, Illinois, July 8-14, 2012|
|Abstract: ||SMAP will be the first Earth science mission to use a deployable 6m mesh reflector for both radar and radiometric measurements from low Earth orbit. The instrument antenna will spin at about 14 rpm, making the design of both reflector and feed more challenging. While the performance requirements imposed by the radar instrument are relatively benign, those pertinent to the radiometer are more difficult to meet. Extreme care was necessary in designing the feed, especially from a performance stability perspective. Thermal variations due to the spacecraft going in and out of eclipse during orbit and direct solar radiation into the horn are just two of the challenges faced during the design phase. In this paper, the basic concepts behind the design of SMAP’s feed will be discussed. Each component of the feed will be analyzed in detail with particular emphasis on its impact on major RF requirements. Overall performance of the feed will also be discussed.|
|Appears in Collections:||JPL TRS 1992+|
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.