Nonsteady behaviour of solar dynamic power systems with Stirling cycle for space stations
In the first part of this paper, a solar dynamic power system with a Stirling engine for space station application is described. Its unsteady behaviour is theoretically modelled and numerically simulated for four representative orbit configurations. The results are compared to that of a solar dynami...
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Veröffentlicht in: | Aerospace science and technology 1999, Vol.3 (1), p.49-58 |
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Format: | Artikel |
Sprache: | eng |
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