Aerospace Contrd and Application ›› 2008, Vol. 34 ›› Issue (2): 18-22.
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Research on On-Orbit Refueling of Maneuverable Platform
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Published:
Abstract:
In view of the characteristics of maneuverable platform, the research on the maneuverable platform refueling on-orbit, which fits to bipropellant systems, is carried out.In the scheme, the surface tension tanks are used as supported and received tanks.The advantages of the scheme are as follows.Firstly, the scheme is matched with the propulsion system of spacecraft in China Secondly, no moving assemblies are used in the scheme, so the reliability of the system can be improved.Thirdly, the surface tension tank is the most appropriate tank for refueling spacecraft on-orbit.In the paper, the refueling system of the maneuverable platform is designed in detail.
Key words:
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CLC Number:
WEI Yanming, PAN Hailin.
Research on On-Orbit Refueling of Maneuverable Platform [J].Aerospace Contrd and Application, 2008, 34(2): 18-22.
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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/
http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2008/V34/I2/18
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