Research Article
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Year 2024, Volume: 1 Issue: 2, 67 - 71, 17.01.2025

Abstract

References

  • Arslantas, E., Bulut, M., & Sözbir, N. (2017). The Effect of Uncertainty Values of Thermal Control System on GEO Satellites. 8th International Conference on Recent Advances in Space Technologies-RAST 2017, Turkish Airforce Academy, Istanbul, Türkiye, 19-22 June.
  • Bulut, M., Sozbir, N., & Gulgonul, S. (2008). Thermal Control Design of TUSAT. 6th International Energy Conversion Engineering Conference (IECEC), Cleveland, OH, USA, July. Bulut, M., Demirel, S., Sozbir, N., & Gulgonul, S. (2008). Battery Thermal Design Conception of Turkish Satellite. 6th International Energy Conversion Engineering Conference (IECEC), Cleveland, OH, USA, July.
  • Bulut, M., Kahriman, A., & Sozbir, N. (2010). Design and Analysis for the Thermal Control System of Nanosatellite, ASME 2010 International Mechanical Congress and Exposition, Vancouver, British Columbia, Canada, 12-18 November.
  • Bulut, M., Kahriman, A., & Sözbir, N. (2010). Uydularda Isıl Kontrol. Termodinamik, (209), 72-78, January.
  • Bulut, M., & Sözbir, N. (2015). Analytical Investigation of a Nanosatellite Panel Surface Temperatures for Different Altitudes and Panel Combinations. Applied Thermal Engineering, 75, 1076-1083.
  • Bulut, M., Sözbir, Ö.R., & Sözbir, N. (2017). Thermal Control of Turksat 3U Nanosatellite. 5th International Symposium on Innovative Technologies in Engineering and Science (ISITES2017) ,Bakü, Azerbaijan, 29-30 September.
  • Bulut, M., & Sozbir, N. (2021). Thermal Design, Analysis and Test Validation of TURKSAT-3USAT. Journal of Thermal Engineering, 7 (3), 468-482.
  • Bulut, M., & Sözbir, N. (2023). A novel approach to estimating dimensions of three-axis stabilized communication satellites with optimal heat transfer. Journal of Thermal Analysis and Calorimetry, 148 (15), 3575-3584 August 2023
  • Chiranjeevi, P.B., Krishnaraj, K., Vinod, K.G., Srinivasan, K., & Sundararajan, T. (2023). Numerical Simulations, Experimental Investigation and Optimization of Hybrid Space Thermal Radiators, Applied Thermal Engineering, 234.
  • Cockfield, R.D. (1968). Structural Optimization of a Space Radiator, Journal Spacecraft Rockets, 5 (10), 1240–1241.
  • Coşkun, H., Bulut, M., & Sözbir, N. (2016). Uydularda optik güneş reflektörü ile ısıl kontrol ve uygulama yöntemi, VI. Ulusal Havacılık ve Uzay Konferansı, Kocaeli Üniversitesi, Kocaeli, Türkiye, 28-30 September.
  • Curran D.G.T., & Lam, T.T. (1996). Weight Optimization for Honeycomb Radiators with Embedded Heat Pipes. Journal of Spacecraft and Rockets, 33 (6), 822-828.
  • Gilmore D.G. (2002). Spacecraft Thermal Control Handbook Vol. 1, 2nd edition. The Aerospace Corporation, CA, USA.
  • Hull, P.V., Tinker, M., SanSoucie, M., & Kittredge, K. (2006). Thermal analysis and shape optimization for an in-space radiator using genetic algorithm. SpaceTechnol. Int. Forum CP813, 81-90.
  • Karam D.R. (1998). Satellite Thermal Control for System Engineers, AIAA, Inc.,VA.
  • Kim, H., Choi, S., Park, S., & Lee, K.Ho. (2015). Node-based Spacecraft Radiator Design Optimization. Advances in Space Research, (55), 1445-1469.
  • Krikkis, R.N., & Razelos, P. (2002). Optimum Design of Spacecraft Radiators with Longitudinal Rectangular and Triangular Fins. Journal of Heat Transfer, (124), 805-811.
  • Liu, T., Sun, Q., Meng, J., Pan, Z., & Tang, Y. (2016). Degradation Modeling of Satellite Thermal Control Coatings in a Low Earth Orbit Environment, Solar Energy, 139, 467-474.
  • Shen, M., Zhang, L., Sun, Z., Kong, L., Liu, Y., & Xue, Z. (2024). Models, Simulations, and Applications of Small Satellite Thermal Analysis, Advances in Space Research, 74 (2), 836-860.
  • Sözbir, N., Bulut, M., Öktem, M.F., & Kahriman, A. (2008). TUSAT haberleşme uydusunun ısıl tasarımı, II. Ulusal Havacılık ve Uzay Konferansı, Istanbul, Türkiye, 15-17 October.
  • Sözbir, N., & Bulut, M. (2009). Türksat haberleşme uydusunun ısıl kontrolü, 17. Ulusal Isı Bilimi ve Tekniği Kongresi, Sivas, Türkiye, 24-27 June.
  • Sozbir, N., & Bulut, M. (2009). Thermal Control of CM and SM Panels for Turkish Satellite, SAE 39th International Conference on Environmental Systems, Savannah, Georgia, USA, 12-16 July.
  • Sozbir, N., Bulut, M., Oktem, M. F., Kahriman, A., & Chaix, A. (2008). Design of Thermal Control Subsystem for TUSAT Telecommunication Satellite. World Academy of Science, Engineering and Technology International Journal of Computer and Systems Engineering, 2(7), 1370-1373.

The Emittance and Absorptance of External Surfaces Values Effect for Payload Panels on Geostationary Orbit Satellite: Thermal Analysis Studies

Year 2024, Volume: 1 Issue: 2, 67 - 71, 17.01.2025

Abstract

One of the most important parameters in the dimensioning stages of communication satellites is the calculation of the areas where the heat to be released into space is located. The satellite thermal control system calculates these areas. Thermal analyses are performed for the north and south panels where the payload equipment is located in three-axis geostationary satellites. It is important to calculate these areas where the heat to be released into space is located correctly. In this study, thermal analysis calculations were performed for a three-axis geostationary satellite with an area of 1 to 10 m2. In the calculations, the absorptance of external surfaces at the end of the satellite's life was calculated by considering 0.27. The radiator area temperature was taken as 30 oC in the calculations.

References

  • Arslantas, E., Bulut, M., & Sözbir, N. (2017). The Effect of Uncertainty Values of Thermal Control System on GEO Satellites. 8th International Conference on Recent Advances in Space Technologies-RAST 2017, Turkish Airforce Academy, Istanbul, Türkiye, 19-22 June.
  • Bulut, M., Sozbir, N., & Gulgonul, S. (2008). Thermal Control Design of TUSAT. 6th International Energy Conversion Engineering Conference (IECEC), Cleveland, OH, USA, July. Bulut, M., Demirel, S., Sozbir, N., & Gulgonul, S. (2008). Battery Thermal Design Conception of Turkish Satellite. 6th International Energy Conversion Engineering Conference (IECEC), Cleveland, OH, USA, July.
  • Bulut, M., Kahriman, A., & Sozbir, N. (2010). Design and Analysis for the Thermal Control System of Nanosatellite, ASME 2010 International Mechanical Congress and Exposition, Vancouver, British Columbia, Canada, 12-18 November.
  • Bulut, M., Kahriman, A., & Sözbir, N. (2010). Uydularda Isıl Kontrol. Termodinamik, (209), 72-78, January.
  • Bulut, M., & Sözbir, N. (2015). Analytical Investigation of a Nanosatellite Panel Surface Temperatures for Different Altitudes and Panel Combinations. Applied Thermal Engineering, 75, 1076-1083.
  • Bulut, M., Sözbir, Ö.R., & Sözbir, N. (2017). Thermal Control of Turksat 3U Nanosatellite. 5th International Symposium on Innovative Technologies in Engineering and Science (ISITES2017) ,Bakü, Azerbaijan, 29-30 September.
  • Bulut, M., & Sozbir, N. (2021). Thermal Design, Analysis and Test Validation of TURKSAT-3USAT. Journal of Thermal Engineering, 7 (3), 468-482.
  • Bulut, M., & Sözbir, N. (2023). A novel approach to estimating dimensions of three-axis stabilized communication satellites with optimal heat transfer. Journal of Thermal Analysis and Calorimetry, 148 (15), 3575-3584 August 2023
  • Chiranjeevi, P.B., Krishnaraj, K., Vinod, K.G., Srinivasan, K., & Sundararajan, T. (2023). Numerical Simulations, Experimental Investigation and Optimization of Hybrid Space Thermal Radiators, Applied Thermal Engineering, 234.
  • Cockfield, R.D. (1968). Structural Optimization of a Space Radiator, Journal Spacecraft Rockets, 5 (10), 1240–1241.
  • Coşkun, H., Bulut, M., & Sözbir, N. (2016). Uydularda optik güneş reflektörü ile ısıl kontrol ve uygulama yöntemi, VI. Ulusal Havacılık ve Uzay Konferansı, Kocaeli Üniversitesi, Kocaeli, Türkiye, 28-30 September.
  • Curran D.G.T., & Lam, T.T. (1996). Weight Optimization for Honeycomb Radiators with Embedded Heat Pipes. Journal of Spacecraft and Rockets, 33 (6), 822-828.
  • Gilmore D.G. (2002). Spacecraft Thermal Control Handbook Vol. 1, 2nd edition. The Aerospace Corporation, CA, USA.
  • Hull, P.V., Tinker, M., SanSoucie, M., & Kittredge, K. (2006). Thermal analysis and shape optimization for an in-space radiator using genetic algorithm. SpaceTechnol. Int. Forum CP813, 81-90.
  • Karam D.R. (1998). Satellite Thermal Control for System Engineers, AIAA, Inc.,VA.
  • Kim, H., Choi, S., Park, S., & Lee, K.Ho. (2015). Node-based Spacecraft Radiator Design Optimization. Advances in Space Research, (55), 1445-1469.
  • Krikkis, R.N., & Razelos, P. (2002). Optimum Design of Spacecraft Radiators with Longitudinal Rectangular and Triangular Fins. Journal of Heat Transfer, (124), 805-811.
  • Liu, T., Sun, Q., Meng, J., Pan, Z., & Tang, Y. (2016). Degradation Modeling of Satellite Thermal Control Coatings in a Low Earth Orbit Environment, Solar Energy, 139, 467-474.
  • Shen, M., Zhang, L., Sun, Z., Kong, L., Liu, Y., & Xue, Z. (2024). Models, Simulations, and Applications of Small Satellite Thermal Analysis, Advances in Space Research, 74 (2), 836-860.
  • Sözbir, N., Bulut, M., Öktem, M.F., & Kahriman, A. (2008). TUSAT haberleşme uydusunun ısıl tasarımı, II. Ulusal Havacılık ve Uzay Konferansı, Istanbul, Türkiye, 15-17 October.
  • Sözbir, N., & Bulut, M. (2009). Türksat haberleşme uydusunun ısıl kontrolü, 17. Ulusal Isı Bilimi ve Tekniği Kongresi, Sivas, Türkiye, 24-27 June.
  • Sozbir, N., & Bulut, M. (2009). Thermal Control of CM and SM Panels for Turkish Satellite, SAE 39th International Conference on Environmental Systems, Savannah, Georgia, USA, 12-16 July.
  • Sozbir, N., Bulut, M., Oktem, M. F., Kahriman, A., & Chaix, A. (2008). Design of Thermal Control Subsystem for TUSAT Telecommunication Satellite. World Academy of Science, Engineering and Technology International Journal of Computer and Systems Engineering, 2(7), 1370-1373.
There are 23 citations in total.

Details

Primary Language English
Subjects Energy
Journal Section Research Article
Authors

Murat Bulut This is me

Nedim Sözbir 0000-0003-4633-2521

Publication Date January 17, 2025
Submission Date November 12, 2024
Acceptance Date January 13, 2025
Published in Issue Year 2024 Volume: 1 Issue: 2

Cite

APA Bulut, M., & Sözbir, N. (2025). The Emittance and Absorptance of External Surfaces Values Effect for Payload Panels on Geostationary Orbit Satellite: Thermal Analysis Studies. Journal of Energy Trends, 1(2), 67-71. https://doi.org/10.5281/zenodo.14670870