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Behavior and relative velocity of debris near geostationary orbit
2010 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

A general model is developed describing third-body gravity perturbation to debris¡¯orbit. Applying this model to debris released from geostationary orbit tells their motion in both short and long term. Without considering the Moon¡¯s precession around the solar pole, the relative velocity between GEO debris can be calculated. This is an important coefficient for simulating the GEO debris environment and can serve as an input to break up models.

Place, publisher, year, edition, pages
2010.
Keyword [en]
Technology, GEO, debris, gravity, perturbation
Keyword [sv]
Teknik
Identifiers
URN: urn:nbn:se:ltu:diva-56564ISRN: LTU-PB-EX--10/048--SELocal ID: d522d642-7c66-4633-9edb-33bd8c62ba1eOAI: oai:DiVA.org:ltu-56564DiVA: diva2:1029951
Subject / course
Student thesis, at least 30 credits
Educational program
Space Engineering, master's level
Examiners
Note
Validerat; 20101217 (root)Available from: 2016-10-04 Created: 2016-10-04Bibliographically approved

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8ea99ad1367ae0261207dcc1c48544139435adb6d16fbd72e58e1c3529448d28878543a4c95266c072128abd642bea971f87f37ca860429718802c19292facf9
Type fulltextMimetype application/pdf

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CiteExportLink to record
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Citation style
  • apa
  • ieee
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  • en-GB
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  • fi-FI
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Output format
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