Hybrid propulsion system for CubeSat applications

The CubeSats platform has become a common basis for the development and flight of very small, low cost spacecraft-particularly amongst University groups. The smallest CubeSats are just 1 litre in volume-comprising a 10.

Bibliographic Details
Main Author:	Ahmed, Ozomata D.
Other Authors:	Knoll, Aaron K.
Published:	University of Surrey 2016
Subjects:	629.4
Online Access:	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701591

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record_format	oai_dc
spelling	ndltd-bl.uk-oai-ethos.bl.uk-7015912018-06-06T15:32:47ZHybrid propulsion system for CubeSat applicationsAhmed, Ozomata D.Knoll, Aaron K.2016The CubeSats platform has become a common basis for the development and flight of very small, low cost spacecraft-particularly amongst University groups. The smallest CubeSats are just 1 litre in volume-comprising a 10.629.4University of Surreyhttp://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701591http://epubs.surrey.ac.uk/812899/Electronic Thesis or Dissertation
collection	NDLTD
sources	NDLTD
topic	629.4
spellingShingle	629.4 Ahmed, Ozomata D. Hybrid propulsion system for CubeSat applications
description	The CubeSats platform has become a common basis for the development and flight of very small, low cost spacecraft-particularly amongst University groups. The smallest CubeSats are just 1 litre in volume-comprising a 10.
author2	Knoll, Aaron K.
author_facet	Knoll, Aaron K. Ahmed, Ozomata D.
author	Ahmed, Ozomata D.
author_sort	Ahmed, Ozomata D.
title	Hybrid propulsion system for CubeSat applications
title_short	Hybrid propulsion system for CubeSat applications
title_full	Hybrid propulsion system for CubeSat applications
title_fullStr	Hybrid propulsion system for CubeSat applications
title_full_unstemmed	Hybrid propulsion system for CubeSat applications
title_sort	hybrid propulsion system for cubesat applications
publisher	University of Surrey
publishDate	2016
url	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.701591
work_keys_str_mv	AT ahmedozomatad hybridpropulsionsystemforcubesatapplications
_version_	1718692233309323264

Hybrid propulsion system for CubeSat applications

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