Araştırma Makalesi
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Yıl 2021, Cilt: 11 Sayı: 1, 29 - 33, 01.06.2021

Öz

Teşekkür

Barışcan KAHRIMAN isimli öğrencime desteklerinden dolayı teşekkür ederim.

Kaynakça

  • V. Braun, “Small Satellite Constellations and End-of-Life Deorbit Considerations.” Handbook of Small Satellites: Technology, Design, Manufacture, Applications, Economics and Regulation, 2019, pp 1-23.
  • C. Bonnal, D. McKnight, C. Phipps, C. Dupont, S. Missonnier, L. Lequette, M. Merle, S. Rommelaere, “Just in Time Collision Avoidance – a Review”. Acta Astronautica, 170, 2020, pp 637-651.
  • A. Chandra, J. Thangavelautham, "De-Orbiting Small Satellites Using Inflatables", in The 19th Advanced Maui Optical and Space Surveillance Technologies Conference. vol. 1 Maui, Hawai, 2018, pp 1-11.
  • "Https://Orbitaldebris.Jsc.Nasa.Gov", (Last access: 25th September 2020)
  • D. J. Kessler, B. G. Cour-Palais, “Collision Frequency of Artificial Satellites: The Creation of a Debris Belt.” Journal of Geophysical Research: Space Physics, 83, 1978, pp 2637-2646.
  • D. McKnight, T. Maclay, “Space Environment Management: A Common Sense Framework for Controlling Orbital.” Debris Risk. Proc. AMOS, 2019.
  • A. Jarry, C. Bonnal, C. Dupont, S. Missonnier, L. Lequette, F. Masson, “Srm Plume: A Candidate as Space Debris Braking System for Just-in-Time Collision Avoidance Maneuver.” Acta Astronautica, 158, 2019, pp 185-197.
  • D. Guglielmo, S. Omar, R. Bevilacqua, L. Fineberg, J. Treptow, B. Poffenberger, Y. Johnson, “Drag Deorbit Device: A New Standard Reentry Actuator for Cubesats.” Journal of Spacecraft and Rockets, 56, 2019, pp 129-145.
  • D. Turse, P. Keller, R. Taylor, M. Reavis, M. Tupper, C. Koehler, "Flight Testing of a Low Cost De-Orbiting Device for Small Satellites.", in The 42nd Aerospace Mechanism Symposium. vol. 1 Greenbelt, Maryland, 2014, pp 183-188.
  • C. R. Phipps, C. Bonnal, “A Spaceborne, Pulsed Uv Laser System for Re-Entering or Nudging Leo Debris, and Re-Orbiting Geo Debris.” Acta Astronautica, 118, 2016, pp 224-236.
  • C. R. Phipps, “L׳Adroit – a Spaceborne Ultraviolet Laser System for Space Debris Clearing.” Acta Astronautica, 104, 2014, pp 243-255.
  • A. Vnukov, T. Balandina, "Effectiveness Analysis of Active Space Debris Removal Technologies for the Geostationary Orbit." International Conference Aviamechanical engineering and transport (AVENT), 2018.
  • S. A. Song, Y. Yoo, C. G. Han, S. Koo, J. Suk, S. Kim, "System Design of Solar Sail Deployment and Its Effect on Attitude Dynamics for Cube Satellite Cnusail-1", The Asia-Pacific International Symposium on Aerospace Technology (APISAT-2014), Shanghai, China, 2014, pp 24-26.
  • “Https://Www.Dupont.Com/Content/Dam/Dupont/Amer/Us/En/Products/Ei-Transformation/Documents/Dec-Kapton-Hn-Datasheet.Pdf", (Last access: 25th September 2020)
  • "Https://Laminatedplastics.Com/Mylar.Pdf", (Last access: 25th September 2020)
  • A. R. Aslan, M. E. Bas, M. S. Uludag, S. Turkoglu, I. E. Akyol, M. D. Aksulu, E. Yakut, M. Suer, B. Karabulut, A. Sofyali, "The Integration and Testing of Beeaglesat", The 6th Nano-Satellite Symposium (NSAT), Kobe, Japan, 2015, pp 1-7.
  • P. Acar, M. Nikbay, A. R. Aslan, "Design Optimization of a 3-Unit Satellite De-Orbiting Mechanism", ESA Small Satellites Systems and Services the 4S Symposium, 2012, pp 4-8.
  • M. Cihan, O. O. Haktanir, I. Akbulut, A. R. Aslan, "Flight Dynamic Analysis of Itupsat1", International Workshop on small satellites, new missions and new technologies, 2008.

DE-ORBITING ELECTRO-MECHANICAL SYSTEM DESIGN FOR MICRO SPACECRAFT

Yıl 2021, Cilt: 11 Sayı: 1, 29 - 33, 01.06.2021

Öz

The number of small and micro satellites in LEO is rapidly increasing. There is a risk of collision due to the lack of active orbital control of these satellites which also raises concerns about the debris. Existing low-orbit satellites pose dangers for new low-orbit satellites to be sent into orbit. A de-orbiting system to be activated at the end of the lifetime of the satellites is seen as the most effective solution to this danger. In this study, an electromagnetic satellite de-orbiting system is designed using aerodynamic principle. This system has been developed for a micro satellite with maximum edge dimensions of 100 cm. When the satellite lifetime is over, the system will be activated and will drop the satellite at the latest of 11 years. This system can de-orbit a micro satellite with a maximum weight of 50 kilograms. This system is activated with a command from the earth after the lifetime of the satellite is over. In this study, a de-orbiting electromechanical system (DES) is designed with an assumption of 750 km of satellite altitude and 98.4 degrees of orbital slope.

Kaynakça

  • V. Braun, “Small Satellite Constellations and End-of-Life Deorbit Considerations.” Handbook of Small Satellites: Technology, Design, Manufacture, Applications, Economics and Regulation, 2019, pp 1-23.
  • C. Bonnal, D. McKnight, C. Phipps, C. Dupont, S. Missonnier, L. Lequette, M. Merle, S. Rommelaere, “Just in Time Collision Avoidance – a Review”. Acta Astronautica, 170, 2020, pp 637-651.
  • A. Chandra, J. Thangavelautham, "De-Orbiting Small Satellites Using Inflatables", in The 19th Advanced Maui Optical and Space Surveillance Technologies Conference. vol. 1 Maui, Hawai, 2018, pp 1-11.
  • "Https://Orbitaldebris.Jsc.Nasa.Gov", (Last access: 25th September 2020)
  • D. J. Kessler, B. G. Cour-Palais, “Collision Frequency of Artificial Satellites: The Creation of a Debris Belt.” Journal of Geophysical Research: Space Physics, 83, 1978, pp 2637-2646.
  • D. McKnight, T. Maclay, “Space Environment Management: A Common Sense Framework for Controlling Orbital.” Debris Risk. Proc. AMOS, 2019.
  • A. Jarry, C. Bonnal, C. Dupont, S. Missonnier, L. Lequette, F. Masson, “Srm Plume: A Candidate as Space Debris Braking System for Just-in-Time Collision Avoidance Maneuver.” Acta Astronautica, 158, 2019, pp 185-197.
  • D. Guglielmo, S. Omar, R. Bevilacqua, L. Fineberg, J. Treptow, B. Poffenberger, Y. Johnson, “Drag Deorbit Device: A New Standard Reentry Actuator for Cubesats.” Journal of Spacecraft and Rockets, 56, 2019, pp 129-145.
  • D. Turse, P. Keller, R. Taylor, M. Reavis, M. Tupper, C. Koehler, "Flight Testing of a Low Cost De-Orbiting Device for Small Satellites.", in The 42nd Aerospace Mechanism Symposium. vol. 1 Greenbelt, Maryland, 2014, pp 183-188.
  • C. R. Phipps, C. Bonnal, “A Spaceborne, Pulsed Uv Laser System for Re-Entering or Nudging Leo Debris, and Re-Orbiting Geo Debris.” Acta Astronautica, 118, 2016, pp 224-236.
  • C. R. Phipps, “L׳Adroit – a Spaceborne Ultraviolet Laser System for Space Debris Clearing.” Acta Astronautica, 104, 2014, pp 243-255.
  • A. Vnukov, T. Balandina, "Effectiveness Analysis of Active Space Debris Removal Technologies for the Geostationary Orbit." International Conference Aviamechanical engineering and transport (AVENT), 2018.
  • S. A. Song, Y. Yoo, C. G. Han, S. Koo, J. Suk, S. Kim, "System Design of Solar Sail Deployment and Its Effect on Attitude Dynamics for Cube Satellite Cnusail-1", The Asia-Pacific International Symposium on Aerospace Technology (APISAT-2014), Shanghai, China, 2014, pp 24-26.
  • “Https://Www.Dupont.Com/Content/Dam/Dupont/Amer/Us/En/Products/Ei-Transformation/Documents/Dec-Kapton-Hn-Datasheet.Pdf", (Last access: 25th September 2020)
  • "Https://Laminatedplastics.Com/Mylar.Pdf", (Last access: 25th September 2020)
  • A. R. Aslan, M. E. Bas, M. S. Uludag, S. Turkoglu, I. E. Akyol, M. D. Aksulu, E. Yakut, M. Suer, B. Karabulut, A. Sofyali, "The Integration and Testing of Beeaglesat", The 6th Nano-Satellite Symposium (NSAT), Kobe, Japan, 2015, pp 1-7.
  • P. Acar, M. Nikbay, A. R. Aslan, "Design Optimization of a 3-Unit Satellite De-Orbiting Mechanism", ESA Small Satellites Systems and Services the 4S Symposium, 2012, pp 4-8.
  • M. Cihan, O. O. Haktanir, I. Akbulut, A. R. Aslan, "Flight Dynamic Analysis of Itupsat1", International Workshop on small satellites, new missions and new technologies, 2008.
Toplam 18 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Elektrik Mühendisliği
Bölüm Araştırma Makalesi
Yazarlar

Uğur Kesen 0000-0003-3460-9060

Yayımlanma Tarihi 1 Haziran 2021
Yayımlandığı Sayı Yıl 2021 Cilt: 11 Sayı: 1

Kaynak Göster

APA Kesen, U. (2021). DE-ORBITING ELECTRO-MECHANICAL SYSTEM DESIGN FOR MICRO SPACECRAFT. European Journal of Technique (EJT), 11(1), 29-33.

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