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

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ReferencesLink to record
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