This paper discusses application of computerassisted design system to development of a solar sail powered spacecraft. Minimum orbit altitude is calculated; also non-linear static analysis for frame-type solar sail is performed in finite elements simulation system. Moreover, mathematical model of small solar sail spacecraft motion is considered. Finally, the analysis of this motion is performed.
The project of the small frame-type solar sail spacecraft
01.06.2015
646208 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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