Study the space debris impact in the early stages of the nano-satellite design

• Autorzy: Mahdi M. C.

Identyfikatory

DOI

10.1515/arsa-2016-0014

• Języki publikacji: EN

Abstrakty

EN

The probability of KufaSat collisions with different sizes of orbital debris and with other satellites which operating in the same orbit during orbital lifetime was determined. Apogee/Perigee Altitude History was used to graph apogee and perigee altitudes over KufaSat lifetime. The required change in velocity for maneuvers necessary to reentry atmospheric within 25 years was calculated. The prediction of orbital lifetime of KufaSat using orbital parameters and engineering specifications as inputs to the Debris Assessment Software (DAS) was done, it has been verified that the orbital lifetime will not be more than 25 years after end of mission which is compatible with recommendation of Inter-Agency Space Debris Coordination Committee (IADC).

Słowa kluczowe

EN

orbital debris mitigation; mission analysis; DAS; KufaSat; IADC; nano-satellite

• Wydawca: Centrum Badań Kosmicznych PAN ; De Gruyter
• Czasopismo: Artificial Satellites : Journal of Planetary Geodesy
• Rocznik: 2016
• Tom: Vol. 51, No. 4
• Strony: 163--172
• Opis fizyczny: Bibliogr. 10 poz., rys., tab.

Twórcy

autor

Mahdi M. C.

• Al-Furat Al-Awsat Technical University, Iraq

Bibliografia

• Committee on Space Derbis, National Research Council. (1995), ORBITAL DEBRIS: A Technical Assessment, National Academies Press.
• International Space University, Floryda Institute of Technology. (2012), Operations and Service Infrastructure for Space Melbourne, Floryda, USA, SSP.
• Inter-Agency Space Derbis Coordination Committee (IADC) Website, Available on http://www.iade-online.org/index.cgi?item=home
• Inter-Agency Space Derbis Coordination Committee (2007) IADC Space Debris Mitigation Guidelines, Revision 1, IDAC-02-01.
• Mahdi M. Chessab (2015) Orbit Design and Simulation on KufaSat Nano-Satellite, Artificial Satellites Journal, Vol. 50, No. 4.
• Mahdi M.C. (2014) Design and Implementation of an Effective Electrifical Power System for Nano-Satellite, International Journal of Scientific&Engineering Research, Volume 5, Issue 5.
• NASA JSC. (January 2014) Orbital Derbis Quarterly News, Volume 18, Issue 1.
• NASA Orbital Debris program Office Orbital Debris Frequently Asked Questions, Available on http://orbitaldebris.jsc.nasa.gov/faq.html#3
• NASA (2012), Debris Assessment Software User’s Guide Version 2.0 Lyndon B. Johnson Space Center, Houston, Texas 77058.
• National Academy of Sciences. (2011) Limiting Future Collision Risk to Spacecraft: An Assessment of NASA's Meteoroid and Orbital Debris Programs, National Academies Press, Washington, D.C.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).