Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites

Bibliographic Details
Main Author:	Sellers, Jerry Jon
Published:	University of Surrey 1986
Subjects:	621.4356 Rocket motors
Online Access:	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201

id	ndltd-bl.uk-oai-ethos.bl.uk-309201
record_format	oai_dc
spelling	ndltd-bl.uk-oai-ethos.bl.uk-3092012015-03-19T08:00:48ZInvestigation into hybrid rockets and other cost-effective propulsion system options for small satellitesSellers, Jerry Jon1986621.4356Rocket motorsUniversity of Surreyhttp://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201Electronic Thesis or Dissertation
collection	NDLTD
sources	NDLTD
topic	621.4356 Rocket motors
spellingShingle	621.4356 Rocket motors Sellers, Jerry Jon Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
author	Sellers, Jerry Jon
author_facet	Sellers, Jerry Jon
author_sort	Sellers, Jerry Jon
title	Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
title_short	Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
title_full	Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
title_fullStr	Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
title_full_unstemmed	Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
title_sort	investigation into hybrid rockets and other cost-effective propulsion system options for small satellites
publisher	University of Surrey
publishDate	1986
url	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201
work_keys_str_mv	AT sellersjerryjon investigationintohybridrocketsandothercosteffectivepropulsionsystemoptionsforsmallsatellites
_version_	1716760540109340672

Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites

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