2018
DOI: 10.1016/j.actaastro.2018.06.036
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Space debris collision probability analysis for proposed global broadband constellations

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Cited by 76 publications
(24 citation statements)
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“…Another private company, OneWeb, intends so launch by the end of 2022 a 648-satellite constellation to provide worldwide internet service as well (Barnett, 2016). Using an evolutionary model with parameters provided by the respective operations application (Barnett, 2016;Space Exploration Holdings, 2016), Le May et al (2018) showed that, within a 5-years operation time, the probability of occurring a catastrophic collision involving an OneWeb spacecraft is ∼5%, whereas the same for SpaceX is near 50%. However, the authors did not consider any effects introduced by solar activity, and, if they did, these figures would have certainly been higher.…”
Section: Discussionmentioning
confidence: 99%
“…Another private company, OneWeb, intends so launch by the end of 2022 a 648-satellite constellation to provide worldwide internet service as well (Barnett, 2016). Using an evolutionary model with parameters provided by the respective operations application (Barnett, 2016;Space Exploration Holdings, 2016), Le May et al (2018) showed that, within a 5-years operation time, the probability of occurring a catastrophic collision involving an OneWeb spacecraft is ∼5%, whereas the same for SpaceX is near 50%. However, the authors did not consider any effects introduced by solar activity, and, if they did, these figures would have certainly been higher.…”
Section: Discussionmentioning
confidence: 99%
“…Despite the congestion and traffic management challenges, FCC filings by SpaceX suggest that collision avoidance manoeuvres can in fact maintain collision-free operations in orbital shells and that the probability of a collision between a non-responsive satellite and tracked debris is negligible. However, the filings do not account for untracked debris 6 , including untracked debris decaying through the shells used by Starlink. Using simple estimates (see “ Methods ”), the probability that a single piece of untracked debris will hit any satellite in the Starlink 550 km shell is about 0.003 after one year.…”
Section: Resultsmentioning
confidence: 99%
“…• míg geostacionárius pályán három megfelelő helyzetű mesterséges holddal szinte globális lefedettség érhető el, addig alacsonyabb pályán nagyszámú műhold szükséges ugyanehhez; • mivel nagyszámú mesterséges hold szükséges adott lefedettség eléréshez, megnő a zsúfoltság, és így az ütközésveszély a szóban forgó tartományban. (A problémával több szakcikk is foglalkozik, például [12] és [13]); • további hátrány, hogy alacsony, illetve nagyon alacsony pályákon (VLEO) a mesterséges holdak passzív élettartama hetekben mérhető a jelentős légköri fékeződés miatt, így a pályamagasság folyamatos korrekcióra szorul, amihez nagy mennyiségű hajtóanyag szükséges; • különösen VLEO esetén kap jelentőséget az oxidáció. Ennek az az oka, hogy ezek a pályák a felső légkörnek a viszonylag sűrű rétegeibe esnek, ahol még számottevő mennyiségű molekuláris és atomos oxigén található.…”
Section: üZemeltetőunclassified