Separable satellite propulsion system configuration
A propulsion system and satellite technology, applied in the field of aerospace, can solve the problems of reducing satellite orbital maintenance efficiency, satellite dullness, and consuming satellite fuel resources, and achieve the effects of improving maintenance efficiency, prolonging on-orbit life, and avoiding dullness
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[0019]In the solutions provided in the embodiments of the present application, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of this application.
[0020]In order to better understand the above technical solutions, the technical solutions of the present application are described in detail below through the accompanying drawings and specific embodiments. It should be understood that the embodiments of the application and the specific features in the embodiments are detailed descriptions of the technical solutions of the present application. It is not a limitation on the technical solutions of the present application. The embodiments of the present application and the technical features in the embodiments can be combined with each other if ...
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