TY - GEN
T1 - Design and Analysis of C-Band Parabolic Antenna Materials for Synthetic Aperture Radar On-Board Microsatellite
AU - Abiwardana, Akbar Danar
AU - Hendrantoro, Gamantyo
AU - Setijadi, Eko
AU - Sumantyo, Josaphat T.S.
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/7/2
Y1 - 2018/7/2
N2 - In developing a synthetic aperture radar onboard a satellite, one component of concern is the antenna. In designing such an antenna, the selection of material types should be considered in order for the effects of expansion and shrinkage due to drastic temperature variations not to result in significant performance changes. In this study, the effect of adoption of various material types to the antenna performance was evaluated when applied to the antenna design by incorporating the changing of dimensions caused by temperature changes through the simulation. The first step involves the making of antenna design using Solidworks, where the design for the reflector is made for various types and material designs. Then a simulated temperature change is performed to find out the change in antenna design dimension to temperature changes that approximate real operating conditions onboard satellite. After that, electromagnetic field for the antenna design before and after heat-induced expansion is simulated to learn antenna performance. Comparison of performances is done to get the best type and material design. From among several designs and types of materials selected, the simulation results show that molybdenum with gold coated design produces the best performance.
AB - In developing a synthetic aperture radar onboard a satellite, one component of concern is the antenna. In designing such an antenna, the selection of material types should be considered in order for the effects of expansion and shrinkage due to drastic temperature variations not to result in significant performance changes. In this study, the effect of adoption of various material types to the antenna performance was evaluated when applied to the antenna design by incorporating the changing of dimensions caused by temperature changes through the simulation. The first step involves the making of antenna design using Solidworks, where the design for the reflector is made for various types and material designs. Then a simulated temperature change is performed to find out the change in antenna design dimension to temperature changes that approximate real operating conditions onboard satellite. After that, electromagnetic field for the antenna design before and after heat-induced expansion is simulated to learn antenna performance. Comparison of performances is done to get the best type and material design. From among several designs and types of materials selected, the simulation results show that molybdenum with gold coated design produces the best performance.
KW - Antenna
KW - heat
KW - material
KW - radar
KW - satellite
UR - http://www.scopus.com/inward/record.url?scp=85066897986&partnerID=8YFLogxK
U2 - 10.1109/ISITIA.2018.8711227
DO - 10.1109/ISITIA.2018.8711227
M3 - Conference contribution
AN - SCOPUS:85066897986
T3 - Proceeding - 2018 International Seminar on Intelligent Technology and Its Application, ISITIA 2018
SP - 15
EP - 18
BT - Proceeding - 2018 International Seminar on Intelligent Technology and Its Application, ISITIA 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 International Seminar on Intelligent Technology and Its Application, ISITIA 2018
Y2 - 30 August 2018 through 31 August 2018
ER -