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Optimizing Thermal Management: An Evaluation of Embedded Aluminum-Ammonia Heat Pipes Honeycomb Sandwich Panel as a Heat Sink for Satellite Use
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This study presents an innovative approach to enhancing thermal management in satellite applications by utilizing an embedded aluminum-ammonia heat pipes honeycomb sandwich panel (HPA-PNL) as a high-performance heat sink. The study focuses on developing and evaluating this advanced heat sink technology, addressing the challenges associated with assessing its performance and suitability for satellite use. The research explores the selection of materials and testing methodologies, highlighting the significance of overcoming existing limitations in the absence of standardized testing methods. The results of the thermal conductivity in Z-directions (KZ) indicated that the areas on top of the heat pipes show higher thermal conductivity than those on top of the honeycomb core. Also, the effect of background heat sources and different kinds of thermal interface material (TIM) on HPA-PNL performance is insignificant. The heat dissipation through the heat pipe is substantial, emphasizing the effective ability to dissipate heat for an HPA-PNL with many heat sources acting simultaneously. The outcomes of this study reveal promising testing methods for evaluating the KZ of the HPA-PNL, proposing the potential of the embedded aluminum-ammonia heat pipes honeycomb sandwich panel as a highly effective and efficient heat sink for satellite systems, thus contributing to the advancement of satellite technology.
Keywords:
honeycomb core panel aluminum ammonia heat pipe heat sink satellite radiatorReferences
- Pisacane, V.L. The Space Environment and Its Effects on Space Systems, 2nd ed.; American Institute of Aeronautics and Astronautics: Reston, US, 2016; pp. 771–852.
- Ponnappan, R.; Donovan, B.; Chow, L. High-power thermal management issues in space-base systems. AIP Conf. Proc. 2002, 608(1), 65–72. https://doi.org/10.1063/1.1449709.
- Mccabe, M.E.; Ku, J.; Benner, S. Design and Testing of a High Power Spacecraft Thermal Management System; National Aeronautics and Space Administration: Washington D.C., US, 1988.
- Darji, J.J. Heat Transfer Through a Honeycomb Sandwich Panel. Master’s thesis, School of Mines and Metallurgy of the University of Missouri, Rolla, Missouri, 1963.
- Nguyen, D.D. Analysis and Testing of Heat Transfer through Honeycomb Panels. Master thesis, California Polytechnic State University, San Luis Obispo, CA, US, May 2012.
- Zohuri, B. Heat Pipe Design and Technology: Modern Applications for Practical Thermal Management, 2nd ed.; Springer International Publishing: AG, Switzerland, 2016.
- Kappe, K.; Bihler, M.; Morawietz, K.; Hügenell, P.P.C.; Pfaff, A.; Hoschke, K. Design Concepts and Performance Characterization of Heat Pipe Wick Structures by LPBF Additive Manufacturing. Materials 2022, 15(24), 8930. https://doi.org/10.3390/ma15248930.
- Tang, H.; Tang, Y.; Li, J.; Sun, Y.; Liang, G.; Peng, R. Experimental Investigation of the Thermal Performance of Heat Pipe with Multi-Heat Source and Double-End Cooling, Appl. Therm. Eng. 2018, 131, 159–166. https://doi.org/10.1016/j.applthermaleng.2017.12.006.
- Fortescue, P.; Swinerd, G.; Stark, J. Spacecraft Systems Engineering, 4th ed.; John Wiley & Sons, Inc.: New York, US, 2011.
- Bejan, A.; Kraus, A.D. Heat Transfer Handbook; John Wiley & Sons, Inc.: New York, US, 2003.
- Stern, T.; Anderson, W.G. High Temperature Lightweight Heat Pipe Panel Technology Development. In Proceeding of the Space Nuclear Conference, San Diego, California, 5–9 June 2005.
- Basiulis, A.; Camarda, C. Design, Fabrication and Test of Liquid Metal Heat-Pipe Sandwich Panels. In Proceeding of the AIAA/ASME 3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference, St. Louis, Missouri, 7–11 June 1982.
- Tanzer, H.J. High Capacity Honeycomb Panel Heat Pipes for Space Radiators. In Proceeding of the AIAA 18th Themophysics Conference, Montreal, Canada, 1–3 June 1983.
- Fabrication and Development of Several Heat Pipe Honeycomb Sandwich Panel Concepts. Available online: https://ntrs.nasa.gov/api/citations/19830002109/downloads/19830002109.pdf.
- Lin, C.L.; Choi, J.H.; Dharant, C.K.H. Thermal Performance of Embedded Heat Pipe Composite Sandwich Panels. In Proceeding of the AIAA 40th Structures, Structural Dynamics, and Materials Conference and Exhibit, St. Louis, Missouri, 12–15 April 1999.