DocumentCode
920668
Title
TECSAR: design considerations and programme status
Author
Sharay, Y. ; Naftaly, U.
Author_Institution
ELTA Electron. Ind. Ltd., Ashdod, Israel
Volume
153
Issue
2
fYear
2006
fDate
4/13/2006 12:00:00 AM
Firstpage
117
Lastpage
121
Abstract
TECSAR is designated to be the first Israeli space-based synthetic aperture radar (SAR) satellite. The system design considerations and the programme status are presented. TECSAR is defined as a space-borne SAR satellite technology demonstration programme. The programme´s purpose is to develop and evaluate the necessary technologies required to achieve high-resolution images combined with large area coverages. These results can be achieved by designing a multi-mode operation, including innovative system and subsystems designed to cope with the special operational requirements and the weight/volume constraints. The TECSAR payload belongs to a family of SAR payloads, developed and produced by ELTA Systems. However, because of the demanding requirements imposed by the potential users and the need to fit into the satellite lightweight bus, TECSAR is unique as far as space SAR is concerned and exhibits the best performances in certain parameters. Mission requirements and system design are described here. The authors focus on the payload and its subsystems and also mention the possibility of multi-polarisation imaging. The TECSAR satellite development phase was completed at the end of 2005.
Keywords
image resolution; radar imaging; radar polarimetry; radar resolution; spaceborne radar; synthetic aperture radar; ELTA system; Israel; TECSAR satellite design; demonstration program status; high-resolution image; innovative system; multimode operation; multipolarisation imaging; space-synthetic aperture radar; subsystem payload; weight-volume constraint;
fLanguage
English
Journal_Title
Radar, Sonar and Navigation, IEE Proceedings -
Publisher
iet
ISSN
1350-2395
Type
jour
DOI
10.1049/ip-rsn:20045124
Filename
1626079
Link To Document