| 摘要 |
The invention concerns a method for thermal control of space equipment which consists in using at least one pumping unit (10, 20) of a pumping assembly comprising at least two series-connected pumping units (10, 20), each pumping unit (10, 20) comprising at least a pump (12, 22) and a valve (14, 24) parallel-connected with each pump (12, 22) so as to short-out said pump (12, 22).
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