PRELIMINARY THERMAL CONTROL DESIGN ANALYSIS OF LAPAN SAR-MICROSATELLITE DEPLOYABLE SOLAR ARRAY PANEL USING ONE NODAL METHODE
DOI:
https://doi.org/10.30536/j.jtd.2019.v17.a3155Keywords:
solar array panels, solar cell, temperature, energyAbstract
LAPAN SAR-Microsatellite is the first LAPAN micro satellite being developed and planned to carry a Synthetic Aperture Radar (SAR) payload. Different from optical satellites that have been developed, LAPAN SAR-Microsatellite requires a lot more power. Solar array panels are needed to generate solar radiation into electrical energy which is used by all of subsystem satellite as energy to turn on and turn off all of components. More larger the area of solar array panel, more greater to the energy obtanied. Therefore, the needed of deployable solar array panel is a must caused by the dimension of the main body structur (MBS) are not large enough. Solar cells will experience a decrease in efficiency if they experience excessive heat. If there is a decrease in efficiency in the solar cell, it will have an impact on the decrease in power produced. The purpose of this study is to conduct thermal design on solar panels to maintain temperature according to their working temperature. Calculations are carried out on the temperature of solar array panel with various optical properties in the upper and lower panel that best which will be use using one nodal analysis methode According to the calculation result from all of the designs passive thermal control system on this study show that Design-5 is the best thermal control design which can be used for LAPAN SAR-microsatellite deployable solar array panel which α=0.24 at the top and ε=0.9 at the bottom surface of solar array panel.References
Almehisni, Reem and Al Naimat, Fadi, 2018. Heat Transfer Influence of Solar Panel on Spacecraft,
Advances in Science and Engineering Technology International Conferences (ASET), Abu Dhabi, United
Arab Emirates.
Boushon, Katelyn Elizabeth, 2018, Thermal analysis and control of small satellites in low Earth orbit,
Masters Theses. 7755.
Das, Tilok K., et al., 2015. A Simple Thermal Design Procedure for Micro and Nano Satellite with
Deployable Solar Array Panel, International Conference on Environtment Systems, Washington.
Gilmore, D.G., 2002, Spacecraft Thermal Control Handbook, El Segundo, Calif.: Aerospace Press, ISSBN:
1-884989-11-X (v.1).
Goueffon, Yann, et al., 2009. Study of Degradation Mechanisms of Black Anodic Films in Simulated
Space Environment. 11th International Symposium on Materials in Space Environment, Aix-en-
Provence, France. pp.0. ffhal-01851864ff, Sep 2009.
Inoue, R., Totani, T., Ogawa, H., Wakita, M., and Nagata, H., 2012. Thermal Analyses and Guideline of
Nano and Micro Satellites on Sun-synchronous Orbits, 4th Nano Satellite Symposium, UN/University of
Tokyo, Nagoya, Japan, 2012.
Li Junlan, Yan Shaoze, Cai Renyu, 2013. Thermal Analysis of Composite Solar Array Subjected to Space
Heat Flux, Aerospace Science and Technology 27, 84-94.
Mitchao, D., Totani T., et al., 2017. Thermal Design and On-orbit Validation of the First Philiphine Micro-
satellite: DIWATA-1, 47th International Conference on Environmental Systems, ICES-2017-130, South
Carolina, July 2017.
Oraby Osama A., El-Kordy Mohamed F., El-Madany Hanaa T., Fahmy Faten H., 2014. UASat Solar Array
Design and Perfomance and Characteristics, International Journal of Science, Engineering and
Technology Research (IJJSETR), Volume 3, Issue 2, February 2014.
R.D. Karam, 1998. Satellite Thermal Control for Systems Engineers. Reston, VA: American Institute of
Aeronautics and Astronautics, Inc, ISBN (print): 978-1-56347-276-3, eISBN: 978-1-60086-652-4.
Septanto, H., Soejana, O., 2018. Simulation Approach to Determine Position of the Fixed Onstalled
Deployable Solar Panel, IEEE ICARES 2018.
Totani, T., Ogawa, H., Inoue, R., Wakita, M., and Nagata, H., 2013. One Nodal Thermal Analysis for Nano
and Micro Satellites on Sun-Synchronous Orbits, Trans. JSASS Aerospace Tech. Japan, Vol. 11, pp. 71-78.
Totani, T., Ogawa, H., Inoue, R., Das, T. K., Wakita, M., and Nagata, H., 2013. Proposal Procedure of
Thermal Design on Micro and Nano Satellites Pointing to Earth, 43rd International Conference on
Environmental Systems, AIAA 2013-3490, Vail, CO, 2013.
Totani, T., Inoue, R., Ogawa, H., Das, T. K., Wakita, M., and Nagata, H., 2014. Thermal Design Procedure
for Micro- and Nano-satellites Pointing to Earth, Journal of Thermodynamics and Heat Transfer, Vol. 28,
No. 3, pp. 524-533.
Totani, T., Inoue, R., Ogawa, H., Das, T. K., Wakita, M., and Nagata, H., 2014. New Procedure for Thermal
Design on Micro- and Nano-satellites Pointing to Earth, Trans. JSASS Aerospace Tech. Japan, Vol. 12, No.
ists29, pp. 11-20.
Triharjanto, R. H., Budiantoro, P. A., Yanto, D., Sumantyo, J. T. S., 2018. The Design Progress of
LAPAN-Chiba University SAR Microsatellite, IEEE ICARES 2018.
Triharjanto, R.H., Budiantoro, P.A., 2018. Stifness Evaluation of LAPAN-A5/ Chibasat Deployable Solar
Panel Composite Plate Using Simplified Finite Element Model, Journal of Aerospace Technology, Vol.16
No.2.
W. K. Tobiska, 2011. The Space Environment, in Space Mission Engineering: The New SMAD, J. R. Wertz,
D. F. Everett, and J. J. Puschell, Eds. Hawthorne, CA: Microcosm Press, pp-127-148.
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2019 Poki Agung Budiantoro, Ahmad Fauzi
This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.
