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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Bibliographic Details
Main Authors PENG ZHEN, WANG WEI, WANG MIN, LI YOUXIA, LI XIUFENG, HAN SHAOHUAN, HU ZHAO
Format Patent
LanguageChinese
English
Published 22.10.2019
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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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
Bibliography:Application Number: CN201910576380