A design and development of pico- and femto-satellites

被引：4

作者：

Alger, M.W.R. ^{[1
]}

Kumar, K.D. ^{[1
]}

机构：

[1] Department of Aerospace Engineering, Ryerson University, Toronto, ON M5B 2K3

来源：

International Journal of Manufacturing Research | 2008年 / 3卷 / 01期

关键词：

CanSat; Cubesat; Femto-satellite; Pico-satellite; Ryf[!sup]3[!/sup]ex; Satellite design; Satellite subsystems;

D O I：

10.1504/IJMR.2008.016452

中图分类号：

学科分类号：

摘要：

The paper presents systematic design and development of pico-satellites focusing on CubeSats. Subsystems of these CubeSats are illustrated through several typical missions that have either been flown or are nearly ready for launch. Furthermore, the authors' recent projects including 'RyCanSat', 'RyPicosat' and 'RyF3ex' are discussed in detail. Finally, future missions involving femto-satellites are presented as a next generation of miniature satellites. © 2008, Inderscience Publishers.

引用

页码：48 / 79

页数：31

共 26 条

[1]

Design of Hardware and Software for the Power Supply for AAU CubeSat, group 002gr733, (2002)

[2]

Alger M., Choudhuri A., CanSat Construction Laboratory Manual, (2006)

[3]

Alminde L., AAU CubeSat, (2003)

[4]

Alminde L., Bisgaard M., Vinther D., Viscor T., Ostergaard K., Robustness of Radio Link Between AAU-Cubesat and Ground Station, (2002)

[5]

Barnhart D., Vladimirova T., Sweeting M., Satellite-on-chip Development for Future Distributed Space Missions, (2006)

[6]

Bleier T., Clarke P., Cutler J., DeMartini L., Dunson C., Flagg S., Lorenz A., Tapio F., Lessons Learned, (2004)

[7]

Caillibot P., Systems Engineering and Ground Station Software for the CanX-2 Nanosatellite, (2005)

[8]

Choudhuri A., ex, (2006)

[9]

Cutler J., AA235 Spacecraft Design Class Notes, (2005)

[10]

Earthquake Research Satellite Demonstrates Ruggedness of Diamond System's CPUs, (2007)

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