Orbit control of a very small satellite using electric propulsion
Miniaturized satellites on a nanosatellite scale below 10kg of total mass contribute most to the number of launched satellites into Low Earth Orbit today. This results from the potential to design, integrate and launch these space missions within months at very low costs. In the past decade, the rel...
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| Format: | Doctoral Thesis |
| Language: | English |
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2021
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| Online Access: | https://opus.bibliothek.uni-wuerzburg.de/frontdoor/index/index/docId/24155 http://nbn-resolving.de/urn:nbn:de:bvb:20-opus-241552 https://nbn-resolving.org/urn:nbn:de:bvb:20-opus-241552 https://doi.org/10.25972/OPUS-24155 https://opus.bibliothek.uni-wuerzburg.de/files/24155/Kramer_Alexander_Dissertation.pdf |
Internet
https://opus.bibliothek.uni-wuerzburg.de/frontdoor/index/index/docId/24155http://nbn-resolving.de/urn:nbn:de:bvb:20-opus-241552
https://nbn-resolving.org/urn:nbn:de:bvb:20-opus-241552
https://doi.org/10.25972/OPUS-24155
https://opus.bibliothek.uni-wuerzburg.de/files/24155/Kramer_Alexander_Dissertation.pdf