Study on Configuration Design of the Multi-Payload Adapter for One Vehicle with Multi-Satellite

Yong Xin Gao; Dong Yang; Qiang Xin; Yin Xin Chen

doi:10.4028/www.scientific.net/AMR.971-973.740

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 971-973Study on Configuration Design of the Multi-Payload...

Study on Configuration Design of the Multi-Payload Adapter for One Vehicle with Multi-Satellite

Abstract:

Constellations of small satellites have a promising use in satellite remote sensing or satellite communication. Launching several small satellites at the same time with one vehicle is a good way to keep the budget of the whole project under control. Multi-payload adapter is an important equipment on the launch vehicle to carry those small satellites during the rising phase and shoot them into their own trajectories during the orbiting phase. The paper studies the relations between the demands of small satellites launching and the multi-payload adapter designing. Also the paper illustrates the necessity of putting the multi-payload adapter into a project and the necessity of researching on the multi-payload concurrent experiment.

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Periodical:

Advanced Materials Research (Volumes 971-973)

Pages:

740-743

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.971-973.740

Citation:

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Online since:

June 2014

Authors:

Yong Xin Gao*, Dong Yang, Qiang Xin, Yin Xin Chen

Keywords:

Configuration, Multi-Payload Adapter, One Vehicle with Multi-Satellite, Small Satellite

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* - Corresponding Author

References

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