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We proposed a new architecture of antenna, transmitter and receiver feeding configuration for small synthetic aperture radar (SAR) that is compatible with 100kg class satellite. Promising applications are constellations of earth observations together with optical sensors, and responsive, disaster monitoring missions. The SAR antenna is a deployable, passive, honeycomb panel antenna with slot array that can be stowed compactly. RF (radio frequency) instruments are in a satellite body and RF signal is fed to a deployable antenna through non-contacting choke flanges at deployable hinges. This paper describes its development strategy and the present development status of the small spaceborne SAR based on this architecture.
Hirobumi SAITO
JAXA
Prilando Rizki AKBAR
JAXA
Hiromi WATANABE
JAXA
Vinay RAVINDRA
JAXA
Jiro HIROKAWA
Tokyo Institite of Technology
Kenji URA
Mitsubishi Electric Corporation
Pyne BUDHADITYA
The University of Tokyo
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Hirobumi SAITO, Prilando Rizki AKBAR, Hiromi WATANABE, Vinay RAVINDRA, Jiro HIROKAWA, Kenji URA, Pyne BUDHADITYA, "Compact X-Band Synthetic Aperture Radar for 100kg Class Satellite" in IEICE TRANSACTIONS on Communications,
vol. E100-B, no. 9, pp. 1653-1660, September 2017, doi: 10.1587/transcom.2016PFI0008.
Abstract: We proposed a new architecture of antenna, transmitter and receiver feeding configuration for small synthetic aperture radar (SAR) that is compatible with 100kg class satellite. Promising applications are constellations of earth observations together with optical sensors, and responsive, disaster monitoring missions. The SAR antenna is a deployable, passive, honeycomb panel antenna with slot array that can be stowed compactly. RF (radio frequency) instruments are in a satellite body and RF signal is fed to a deployable antenna through non-contacting choke flanges at deployable hinges. This paper describes its development strategy and the present development status of the small spaceborne SAR based on this architecture.
URL: https://global.ieice.org/en_transactions/communications/10.1587/transcom.2016PFI0008/_p
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@ARTICLE{e100-b_9_1653,
author={Hirobumi SAITO, Prilando Rizki AKBAR, Hiromi WATANABE, Vinay RAVINDRA, Jiro HIROKAWA, Kenji URA, Pyne BUDHADITYA, },
journal={IEICE TRANSACTIONS on Communications},
title={Compact X-Band Synthetic Aperture Radar for 100kg Class Satellite},
year={2017},
volume={E100-B},
number={9},
pages={1653-1660},
abstract={We proposed a new architecture of antenna, transmitter and receiver feeding configuration for small synthetic aperture radar (SAR) that is compatible with 100kg class satellite. Promising applications are constellations of earth observations together with optical sensors, and responsive, disaster monitoring missions. The SAR antenna is a deployable, passive, honeycomb panel antenna with slot array that can be stowed compactly. RF (radio frequency) instruments are in a satellite body and RF signal is fed to a deployable antenna through non-contacting choke flanges at deployable hinges. This paper describes its development strategy and the present development status of the small spaceborne SAR based on this architecture.},
keywords={},
doi={10.1587/transcom.2016PFI0008},
ISSN={1745-1345},
month={September},}
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TY - JOUR
TI - Compact X-Band Synthetic Aperture Radar for 100kg Class Satellite
T2 - IEICE TRANSACTIONS on Communications
SP - 1653
EP - 1660
AU - Hirobumi SAITO
AU - Prilando Rizki AKBAR
AU - Hiromi WATANABE
AU - Vinay RAVINDRA
AU - Jiro HIROKAWA
AU - Kenji URA
AU - Pyne BUDHADITYA
PY - 2017
DO - 10.1587/transcom.2016PFI0008
JO - IEICE TRANSACTIONS on Communications
SN - 1745-1345
VL - E100-B
IS - 9
JA - IEICE TRANSACTIONS on Communications
Y1 - September 2017
AB - We proposed a new architecture of antenna, transmitter and receiver feeding configuration for small synthetic aperture radar (SAR) that is compatible with 100kg class satellite. Promising applications are constellations of earth observations together with optical sensors, and responsive, disaster monitoring missions. The SAR antenna is a deployable, passive, honeycomb panel antenna with slot array that can be stowed compactly. RF (radio frequency) instruments are in a satellite body and RF signal is fed to a deployable antenna through non-contacting choke flanges at deployable hinges. This paper describes its development strategy and the present development status of the small spaceborne SAR based on this architecture.
ER -