Selection of project structure for nanosatellite propulsion system
This paper presents the results of theoretical and experimental research of a prototype of a propulsion system for periodical low-Earth orbit correction of research-and-educational nanosatellites. For that purpose, the prototype is to provide at least 20 m/s relative velocity for a 3U CubeSat with a...
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| Autori principali: | , , , , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Samara National Research University
2019-10-01
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| Serie: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
| Soggetti: | |
| Accesso online: | https://journals.ssau.ru/index.php/vestnik/article/view/7451 |
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