Silicon solid-state small satellite design based on IC and MEMS

Author

Xuwen, Liang ; Li, Li ; Huawang, Li ; Yinjian, Chen ; Shen Dexin ; Genqing, Yang

Author_Institution

Inst. of Metall., Acad. Sinica, Shanghai, China

fYear

1998

fDate

1998

Firstpage

932

Lastpage

935

Abstract

Silicon solid-state small satellite (or nano satellite) is a new kind of aerospace aircraft, which adopts ideas greatly different from the conventional method. The small satellite is composed of ASIMs, which make the conventional complex system into a single system with IC and MEMS technologies. The fundamental principle of how to improve the silicon-solid state small satellite is discussed, as well as its application in special data store and forward communication. We also introduce our research on MEMS application in space. A practical design of a data communication nano satellite about 15 kG in weight and 10 inch in line length is also given

Keywords

artificial satellites; attitude control; attitude measurement; micromechanical devices; micropumps; microsensors; microvalves; satellite communication; silicon; 10 inch; 15 kg; ASIMs; IC based; MEMS based; Si; control; data communication satellite; forward communication; micro propulsion; microsensor system; nano satellite; small satellite design; solid-state small satellite; star sensor; Aerospace electronics; Artificial satellites; Communication system control; Control systems; Micromechanical devices; Satellite broadcasting; Silicon; Solid state circuits; Space technology; Telecommunication control;

fLanguage

English

Publisher

ieee

Conference_Titel

Solid-State and Integrated Circuit Technology, 1998. Proceedings. 1998 5th International Conference on

Conference_Location

Beijing

Print_ISBN

0-7803-4306-9

Type

conf

DOI

10.1109/ICSICT.1998.786529

Filename

786529