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Year 2019, Volume: 23 Issue: 5, 986 - 992, 01.10.2019
https://doi.org/10.16984/saufenbilder.546894

Abstract

References

  • [1] L. Yang, Q. Li, L. Kong, S. Gu and L. Zhang, “Quasi-all-passive thermal control system design and on-orbit validation of Luojia 1-01 satellite,” Sensors, vol. 19, pp. 827-18.
  • [2] D. Curran and T.T. Lam, “Weight optimization for honeycomb radiators with embedded heat pipes,” Journal of Spacecraft and Rockets, vol. 33, pp. 822-828, 1996.
  • [3] K.F.C.H. Sam and Z. Deng, “Optimization of a space based radiator, ” Applied Thermal Engineering, vol.31, pp. 2312-2320, 2011.
  • [4] C. Arslanturk, “Optimum design of space radiators with temperature-dependent thermal conductivity,” Applied Thermal Engineering, vol. 26, no. 17-18, pp. 1149-1157, 2006.
  • [5] R.D. Cockfield, “Structural optimization of a space radiator,” Journal of Spacecraft and Rockets, vol. 5, no. 10, pp. 1240-1241, 1968.
  • [6] W.H. Kelly and Jr. J.H. Reisenweber 1982, “Optimization of a radiator heat pipe radiator for spacecraft high-power TWTAs,” Advances in Heat Pipe Technology, Proceedings of the IVth International Heat Pipe Conference, London, UK, 1981.
  • [7] I. Muraoka, R.L. Galski, F.L De Sousa and F.M. Ramos, “Stochastic spacecraft thermal design optimization with low computational cost,” Journal of Spacecraft and Rockets, vol. 43, no. 6, 2006.
  • [8] P.V. Hull, M. Tinker, M. SanSoucie, K. Kittredge, Thermal analysis and shape optimization of an in-space radiator using genetic algorithms, AIP Conference Proceedings 813 (81), 2006.
  • [9] H.K. Kim, S. Choi, S.O. Park and K.H. Lee, “Node-based spacecraft radiator design optimization,” Advances in Space Research, vol. 55, no. 5, pp. 1445-1469, 2015.
  • [10] T. Y. Kim, S. Chang and S. S. Young, “Optimizing the design of space radiators for thermal performance and mass reduction,” Journal of Aerospace Engineering, vol. 30, no. 3, 04016090-1- 04016090-6.
  • [11] A.D. Willams and S.E. Palo ,“Issues and Implications of the Thermal Control Systems on the ‘ six day spacecraft’, ” in: 4th Responsive Space Conference, RS4-2006-6001, Los Angeles, California, USA, 2006.
  • [12] B. Pattan, Satellite Systems Principles and Technologies, New York, NY, Van Nostrand Reinhold; 1993, ISBN-13: 978-0442013578
  • [13] M. G. Boato, E.C. Garcia, M.B. Dos Santos and A.F. Beloto, “Assembly and Testing of a Thermal Control Component Developed in Brazil,” Journal of Aerospace Technology and Management, vol.9. no.2, 2017.
  • [14] D.B. DeBra and E. Gottzein “Automatic Control in Aerospace 1992,” the 12th IFAC Symposium, Ottobrunn, Germany, 1992.
  • [15] Alcatel Alenia Space, Space Engineering & Operations University, AOCS Attitude and Orbit Control Subsystem Spacecraft Introduction Session, Ref: 200203304L Issue 1, 2005.
  • [16] M. Bulut and N.Sozbir “Analytical investigation of a nanosatellite panel surface temperatures for different altitudes and panel combinations,” Applied Thermal Engineering, vol. 75, pp. 1076-1083, 2015.
  • [17] M. Bulut, “Thermal simulation software based on excel for spacecraft applications,” Selcuk University Journal of Engineering ,Science and Technology, vol. 6, no. 7, pp. 596-600, 2018.
  • [18] M. Bulut and N. Sozbir, “Heat rejection capability for geostationary satellites,” 9th Ankara International Aerospace Conference (AIAC 2017), METU, Ankara, Turkey, 2017.
  • [19] K.F.C.H. Sam and D. Zhongmin, “Optimization of a space based radiator,” Applied Thermal Engineering, vol. 31, pp. 2312-2320, 2011.

Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach

Year 2019, Volume: 23 Issue: 5, 986 - 992, 01.10.2019
https://doi.org/10.16984/saufenbilder.546894

Abstract





Determining
radiative areas of geostationary satellite are one of the challenging tasks for
satellite thermal engineers at the early stage of the project. Radiative areas
of geostationary communication satellite for the payload and platform panels
are determined based on worst hot case (end-of-life). After calculation of radiative
areas, it needs to be optimized according to worst hot and cold scenario at sun
acquisition mode, orbit raising mode and geostationary orbit. In this study,
geostationary satellite platform panel was considered. The radiator’s dimensions
were calculated and then optimized based on
sun acquisition mode, orbit raising
mode and geostationary orbit. Calculated radiative areas both the north panel
and the south panel was 1 m2. Radiative areas were studied at +/-10%
m2. It was seen from the analytical results that the surface
temperature of the platform panel areas were between -48.5 oC at 1.1
m2 of radiative area and 37.7 oC at 0.9 m2 of
radiative area.

References

  • [1] L. Yang, Q. Li, L. Kong, S. Gu and L. Zhang, “Quasi-all-passive thermal control system design and on-orbit validation of Luojia 1-01 satellite,” Sensors, vol. 19, pp. 827-18.
  • [2] D. Curran and T.T. Lam, “Weight optimization for honeycomb radiators with embedded heat pipes,” Journal of Spacecraft and Rockets, vol. 33, pp. 822-828, 1996.
  • [3] K.F.C.H. Sam and Z. Deng, “Optimization of a space based radiator, ” Applied Thermal Engineering, vol.31, pp. 2312-2320, 2011.
  • [4] C. Arslanturk, “Optimum design of space radiators with temperature-dependent thermal conductivity,” Applied Thermal Engineering, vol. 26, no. 17-18, pp. 1149-1157, 2006.
  • [5] R.D. Cockfield, “Structural optimization of a space radiator,” Journal of Spacecraft and Rockets, vol. 5, no. 10, pp. 1240-1241, 1968.
  • [6] W.H. Kelly and Jr. J.H. Reisenweber 1982, “Optimization of a radiator heat pipe radiator for spacecraft high-power TWTAs,” Advances in Heat Pipe Technology, Proceedings of the IVth International Heat Pipe Conference, London, UK, 1981.
  • [7] I. Muraoka, R.L. Galski, F.L De Sousa and F.M. Ramos, “Stochastic spacecraft thermal design optimization with low computational cost,” Journal of Spacecraft and Rockets, vol. 43, no. 6, 2006.
  • [8] P.V. Hull, M. Tinker, M. SanSoucie, K. Kittredge, Thermal analysis and shape optimization of an in-space radiator using genetic algorithms, AIP Conference Proceedings 813 (81), 2006.
  • [9] H.K. Kim, S. Choi, S.O. Park and K.H. Lee, “Node-based spacecraft radiator design optimization,” Advances in Space Research, vol. 55, no. 5, pp. 1445-1469, 2015.
  • [10] T. Y. Kim, S. Chang and S. S. Young, “Optimizing the design of space radiators for thermal performance and mass reduction,” Journal of Aerospace Engineering, vol. 30, no. 3, 04016090-1- 04016090-6.
  • [11] A.D. Willams and S.E. Palo ,“Issues and Implications of the Thermal Control Systems on the ‘ six day spacecraft’, ” in: 4th Responsive Space Conference, RS4-2006-6001, Los Angeles, California, USA, 2006.
  • [12] B. Pattan, Satellite Systems Principles and Technologies, New York, NY, Van Nostrand Reinhold; 1993, ISBN-13: 978-0442013578
  • [13] M. G. Boato, E.C. Garcia, M.B. Dos Santos and A.F. Beloto, “Assembly and Testing of a Thermal Control Component Developed in Brazil,” Journal of Aerospace Technology and Management, vol.9. no.2, 2017.
  • [14] D.B. DeBra and E. Gottzein “Automatic Control in Aerospace 1992,” the 12th IFAC Symposium, Ottobrunn, Germany, 1992.
  • [15] Alcatel Alenia Space, Space Engineering & Operations University, AOCS Attitude and Orbit Control Subsystem Spacecraft Introduction Session, Ref: 200203304L Issue 1, 2005.
  • [16] M. Bulut and N.Sozbir “Analytical investigation of a nanosatellite panel surface temperatures for different altitudes and panel combinations,” Applied Thermal Engineering, vol. 75, pp. 1076-1083, 2015.
  • [17] M. Bulut, “Thermal simulation software based on excel for spacecraft applications,” Selcuk University Journal of Engineering ,Science and Technology, vol. 6, no. 7, pp. 596-600, 2018.
  • [18] M. Bulut and N. Sozbir, “Heat rejection capability for geostationary satellites,” 9th Ankara International Aerospace Conference (AIAC 2017), METU, Ankara, Turkey, 2017.
  • [19] K.F.C.H. Sam and D. Zhongmin, “Optimization of a space based radiator,” Applied Thermal Engineering, vol. 31, pp. 2312-2320, 2011.
There are 19 citations in total.

Details

Primary Language English
Subjects Mechanical Engineering
Journal Section Research Articles
Authors

Murat Bulut 0000-0002-9024-7722

Nedim Sözbir 0000-0003-4633-2521

Publication Date October 1, 2019
Submission Date March 29, 2019
Acceptance Date June 17, 2019
Published in Issue Year 2019 Volume: 23 Issue: 5

Cite

APA Bulut, M., & Sözbir, N. (2019). Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach. Sakarya University Journal of Science, 23(5), 986-992. https://doi.org/10.16984/saufenbilder.546894
AMA Bulut M, Sözbir N. Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach. SAUJS. October 2019;23(5):986-992. doi:10.16984/saufenbilder.546894
Chicago Bulut, Murat, and Nedim Sözbir. “Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach”. Sakarya University Journal of Science 23, no. 5 (October 2019): 986-92. https://doi.org/10.16984/saufenbilder.546894.
EndNote Bulut M, Sözbir N (October 1, 2019) Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach. Sakarya University Journal of Science 23 5 986–992.
IEEE M. Bulut and N. Sözbir, “Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach”, SAUJS, vol. 23, no. 5, pp. 986–992, 2019, doi: 10.16984/saufenbilder.546894.
ISNAD Bulut, Murat - Sözbir, Nedim. “Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach”. Sakarya University Journal of Science 23/5 (October 2019), 986-992. https://doi.org/10.16984/saufenbilder.546894.
JAMA Bulut M, Sözbir N. Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach. SAUJS. 2019;23:986–992.
MLA Bulut, Murat and Nedim Sözbir. “Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach”. Sakarya University Journal of Science, vol. 23, no. 5, 2019, pp. 986-92, doi:10.16984/saufenbilder.546894.
Vancouver Bulut M, Sözbir N. Optimized Analytical Solution of Platform Panel Radiative Area Dimensioning of Geostationary Communications Satellites: A Practical Approach. SAUJS. 2019;23(5):986-92.