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6U CubeSat commercial applications

Published online by Cambridge University Press:  27 January 2016

S. R. Tsitas  and
J. Kingston
J. Kingston*
Affiliation:
Cranfield Space Research Centre, Aerospace Engineering Department, Cranfield University, UK
*
j.kingston@cranfield.ac.uk
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Abstract

Recent work by Tsitas and Kingston(1) has demonstrated that an 8kg 6U CubeSat can be designed to perform Earth observation missions equivalent to those of 50-150kg microsatellites. Their design is reviewed and its commercial potential is compared to the 156kg RapidEye spacecraft. Three other commercial applications of this design are described. These are: a standard spacecraft for space scientists and astronomers; the spacecraft component of an N nation 5 spectral band disaster monitoring constellation and a night imaging satellite. Nanosatellites should now be considered for commercial missions previously thought to require microsatellites.

Type
Research Article
Information
The Aeronautical Journal , Volume 116 , Issue 1176 , February 2012 , pp. 189 - 198
Copyright
Copyright © Royal Aeronautical Society 2012 

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References

1. Tsitas, S. and Kingston, J. 6U CubeSat design for Earth observation with 6.5m GSD, 5 Spectral Bands and 14 Mbps downlink, Aeronaut J, November 2010, 114, (1161), pp 689–697.Google Scholar
2. ISO/TC 20/SC 14/WG 3, Space systems — Determining orbit lifetime, ISO/DIS/27852, 2009 <http://aiaa.kavi.com/apps/group_public/download.php/1973/20090605_ISO_27852_(G)_Orbit_Lifetime.pdf> >Google Scholar
3. The RapidEye Mission, 2007, <http://wgiss.ceos.org/meetings/wgiss24/Host%20Workshop/RapidEye _WGISS_Oct2007.pdf> >Google Scholar
4. RapidEye: A commodities view From 60,000 feet, 2007, <http://www.rapideye.de/upload/In%20the%20News/HedgeworldJuly07.pdf> >Google Scholar
5. Dnepr — Specifications, Space and Tech, <http://www.spaceandtech.com/spacedata/elvs/dnepr_specs.shtml> >Google Scholar
6. Small-satellite costs, 2001, Crosslink, <http://www.aero.org/publications/crosslink/winter2001/04.html> >Google Scholar
7. SpaceX, 2011, <http://www.spacex.com/falcon1.php> >Google Scholar
8. National Science Foundation, CubeSat-based Science Missions for Space Weather and Atmospheric Research, 2008 <http://www.nsf.gov/pubs/2008/nsf08549/nsf08549.htm> >Google Scholar
9. Maxwell Technologies, Datasheet BC Power Series Radial D Cell 310F, Ultracapacitor <http://www.maxwell.com/products/ultracapacitors/docs/DATASHEET_D_CELLS_1017105.PDF> >Google Scholar
10. Clyde Space, User Manual: Standalone 30Wh Battery, 2010, Document No: C3-USM-5016-CS-BAT-30Wh<http://www.clyde-space.com/documents/1902> >Google Scholar
11. Aguttes, J.P. High resolution (metric) SAR microsatellite, based on the CNES MYRIADE bus, Geoscience and Remote Sensing Symposium (IGARSS 01), IEEE 2001 Int, 2001, 1, pp224–226.Google Scholar
12. Busazi, D., Catanzarite, J., Laher, R., Conrow, T., Shupe, D., Gautier, T.N., Kreidl, T. and Everett, D. The detection of multimodal oscillations on α Ursae Majoris,Astrophysical J, April 2000, 1, (532), L133–L136.Google Scholar
13. Zee, R. and Stibrany, P., Canada’s first microsatellite — an enabling low-cost technology for future space science and technology missions, Canadian Aeronautics and Space J, 48, (1), pp 1–11.Google Scholar
14. Grocott, S.C.O. and Carroll, K.A. Arc-second attitude control for the NESS asteroid/satellite tracking microsat, <http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.133.7848&rep=rep1&type=pdf> >Google Scholar
15. Surrey Satellite Technology Ltd, Surrey Missions: DMC Disaster Monitoring Constellation, <http://centaur.sstl. co.uk/datasheets/Mission_DMC.pdf> >Google Scholar
16. Curiel, A., Boland, L., Cooksley, J., Bekhti, M., Stephens, P., Sun, W. and Sweeting, M. First results from the disaster monitoring constellation (DMC), Acta Astronautica, 2005, 56, pp 261–271.Google Scholar
17. Elvidge, C.D., Cinzano, P., Pettit, D.R., Arvesen, J., Sutton, P., Small, C., Newman, R., Longcore, T., Rich, C., Safran, J., Weeks, J. and Ebener, S. The Nightsat mission concept, Int J Remote Sensing, 2007, 28, pp 2645–2670.Google Scholar
18. Fairchild Imaging, 2009, <http://www.fairchildimaging.com/documents/CCD5061DataSheetRevB_004.pdf> >Google Scholar
19. Hamamatsu, TDI-CCD image sensors, 2009. <http://sales.hamamatsu.com/assets/pdf/parts_S/s1020002_etc_kmpd1098e04.pdf> >Google Scholar
20. LN-200S Inertial Measurement Unit <ftp://ftp.uni-duisburg.de/Hardware/Litton/Prodsheet_LN200S.pdf> >Google Scholar
21. Nightsat Mission Overview, 2008, < http://files.harc.edu/Documents/Announcements/2008/NightSat.pdf> >Google Scholar