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Satellites are used for navigation, communication, oceanography, astronomy, etc.. Satellites come in a diversity of sizes and forms. Depending on the satellite’s mission, different subsystems are used. These subsystems are installed inside a housing to protect them from the space environment. This housing, which is also known as the satellite primary structure or mechanical structure, is made of durable materials that can endure severe conditions during launch and in the orbit. The optimisation of satellite mass is crucial right now since satellites are losing mass every day to reduce the cost of manufacturing and launching. This review first introduces an overview of the satellite classifications and subsystems. Then, the different types of mechanical load analysis the satellite subjects itself to are demonstrated. The advanced approaches for promoting the performance of the mechanical structures of satellites are explored, with a spotlight on the effect of the optimisation parameters of isogrid and honeycomb sandwich structures on the mechanical performance of the satellite primary structure. The assembly, integration and testing (AIT) of the small satellite are briefly presented. Finally, the important potential designs to improve the mechanical performance of the satellite primary structure and the challenges of further research are summarised.
Czasopismo
Rocznik
Tom
Strony
40--54
Opis fizyczny
Bibliogr. 53 poz., fot., rys.
Twórcy
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
autor
- Mechanical Design and Production Engineering Division, Mechanical Engineering Department, Faculty of Engineering, Suez University, Suez 43512, Egypt
Bibliografia
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- [28] Ciccarelli, Daniele, Forcellese, Archimede, Greco, Luciano, Mancia, Tommaso, Pieralisi, Massimiliano, Simoncini, Michela, and Vita, Alessio. “Buckling Behavior of 3D Printed Composite Isogrid Structures.” Procedia CIRP Vol. 99 (2021): pp. 375-380.
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- [30] Zheng, Q., Jiang, D., Huang, C., Shang, X., and Ju, S. “Analysis of Failure Loads and Optimal Design of Composite Lattice Cylinder under Axial Compression.” Composite Structures Vol. 131 (2015): pp. 885-894.
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- [32] Rahimi, G.H., Zandi, M., and Rasouli, S.F. “Analysis of the Effect of Stiffener Profile on Buckling Strength in Composite Isogrid Stiffened Shell Under Axial Loading”. Aerospace Science and Technology Vol. 24 (2013): pp. 198-203.
- [33] Dawood, Sarmad Daood Salman, Inayatullah, Othman B., and Samin, Razali B. “Computational Study of the Effect of using Open Isogrids on the Natural Frequencies of a Small Satellite Structure.” Acta Astronautica Vol. 106 (2015): pp. 120-138.
- [34] Forcellese, Archimede, di Pompeo, Valerio, Simoncini, Michela, and Vita, Alessio. “Manufacturing of Isogrid Composite Structures by 3D Printing”. Procedia Manufacturing Vol. 47 (2020): pp. 1096-1100.
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- [41] Li, Z.G., Wang, J.M., Li, M., and Chen, F.Y. “Theoretical Analysis and Numerical Simulation of Square Honeycombs.” Journal of Physics: Conference Series Vol. 1777 (2021): p. 012042.
- [42] Thomas, Tiju, and Tiwari, Gaurav. “Crushing Behavior of Honeycomb Structure: A Review.” International Journal of Crashworthiness Vol. 24 No. 5 (2019): pp. 555-579.
- [43] Abdelal, Gasser F., Abuelfoutouh, Nader, and Gad, Ahmed H. Finite Element Analysis for Satellite Structures. Springer-Verlag, London (2013), DOI 10.1007/978-1-4471-4637-7.
- [44] Yilmaz, Fatih, Haktanir, Ozan, and Uygur, Ahmet. “Quasi-Static Structural Test of Satellites.” Conference Paper, 2015, DOI: 10.1109/rASt.2015.7208381.
- [45] Raviprasad, Srikanth, and Nayak, Nagaraj. “Dynamic Analysis and Verification of Structurally Optimized Nano-Satellite Systems.” Journal of Aerospace Science and Technology Vol. 1 (2015): pp. 78-90.
- [46] NASA Engineering and Safety Center Technical Bulletin No. 15-03, Best Practices for Use of Sine Vibration Testing.
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- [48] Souto, Carlos, and Pirk, Rogerio. “Acoustic Loads on a Sounding Rocket Lift-Off ”.19th Brazilian Congress of Mechanical Engineering, Proceedings of COBEM, 2007.
- [49] Pisacane, V. Fundamentals of Space Systems. 2 nd edn. Oxford University Press, New York (2005).
- [50] Sebestyen, George, Fujikawa, Steve, Galassi, Nicholas, and Chuchra, Alex. Low Earth Orbit Satellite Design. Microcosm Press and Springe (2018), DOI 10.1007/978-3-319-68315-7.
- [51] Baghal, Lisa. “Assembly, Integration, and Test Methods for Operationally Responsive Space Satellites.” Master Thesis, Corpus ID: 108725233. 2010.
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Uwagi
1. Błędnie przypisany ORCID Refaey Ahmed.
2. Opracowanie rekordu ze środków MNiSW, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-be20e79e-cafd-47f0-a311-3c5c2fb3125e