DocumentCode
2946500
Title
A 6-m mesh reflector antenna for SMAP: Modeling the RF performance of a challenging Earth-orbiting instrument
Author
Focardi, P. ; Brown, P. ; Rahmat-Samii, Y.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
2011
fDate
3-8 July 2011
Firstpage
2987
Lastpage
2990
Abstract
A complete and accurate RF model of the SMAP observatory has been presented in this paper. Extreme care has been used in modeling all the important parts of the spacecraft to provide reliable information about the performance of the instrument under various conditions. An ongoing work of RF model refinement based on the constant development of the spacecraft and instrument is also being carried on to keep the model up to date. Field of view studies have been performed and mechanical and thermal deformations are also being considered. Since radiation pattern measurements of the actual antenna are not planned, the development of this RF model represents a very important milestone for the mission.
Keywords
aerospace instrumentation; aircraft antennas; antenna radiation patterns; net structures (mechanical); reflector antennas; Earth orbiting instrument; RF performance modeling; SMAP observatory; mesh reflector antenna; size 6 m; Antenna measurements; Antenna radiation patterns; Instruments; Radio frequency; Radiometry; Space vehicles; Thermal stability; Earth Science; RF modeling; deployable antennas; mesh reflectors; reflector antennas; remote sensing;
fLanguage
English
Publisher
ieee
Conference_Titel
Antennas and Propagation (APSURSI), 2011 IEEE International Symposium on
Conference_Location
Spokane, WA
ISSN
1522-3965
Print_ISBN
978-1-4244-9562-7
Type
conf
DOI
10.1109/APS.2011.5997157
Filename
5997157
Link To Document