Full-electric-push satellite platform configuration based on one-rocket two-satellite self-series-connection launching mode
The invention disclose a full-electric-push satellite platform configuration based on a one-rocket two-satellite self-series-connection launching mode. The full-electric-push satellite platform configuration comprises two sub-satellite platforms with the same structure and a connecting and separatin...
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Main Authors | , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
22.10.2019
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Subjects | |
Online Access | Get full text |
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Summary: | The invention disclose a full-electric-push satellite platform configuration based on a one-rocket two-satellite self-series-connection launching mode. The full-electric-push satellite platform configuration comprises two sub-satellite platforms with the same structure and a connecting and separating device (61), the connecting and separating device (61) is installed at one end of a center force bearing cylinder (121) and penetrates through a -Z plate (122) of one sub-satellite platform to be connected to a +Z plate (111) of the other sub-satellite platform. According to the full-electric-pushsatellite platform configuration, through the structure optimization design and the connecting and separating device, one-rocket two-satellite self-series-connection launching is realized; meanwhile,the two-cabin configuration, the load and platform equipment comprehensive layout and the storage battery and electric thruster innovative layout are adopted, so that on-satellite resource sharing isrealized, the testing proc |
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Bibliography: | Application Number: CN201910576380 |