Investigations of a combustible inertial launch design

dc.contributor.author	Yemets, V.
dc.contributor.author	Prince, Simon A.
dc.contributor.author	Wilkinson, Ray
dc.date.accessioned	2020-03-11T16:31:13Z
dc.date.available	2020-03-11T16:31:13Z
dc.date.issued	2015-06-30
dc.description.abstract	The paper develops a subject of a combustible inertial (self-feeding) launch vehicle for nano and pico satellites. A part of the paper considers a flight of the rocket using ballistic, aerodynamic and thermal calculations. Another part describes experimental investigations of a laboratory-scale model of the rocket engine. Plans for future work and prospects of the self-feeding technology combined with pulse engine mode for microlaunchers and small satellite micro propulsion concludes the paper.	en_UK
dc.identifier.citation	Yemets V, Prince SA, Wilkinson R. (2015) Investigations of a combustible inertial launch design. Journal of the British Interplanetary Society, Volume 68, Issue 7, pp. 188-199	en_UK
dc.identifier.issn	0007-084X
dc.identifier.uri	https://www.jbis.org.uk/paper/2015.68.188
dc.identifier.uri	https://dspace.lib.cranfield.ac.uk/handle/1826/15274
dc.language.iso	en	en_UK
dc.publisher	British Interplanetary Society	en_UK
dc.rights	Attribution-NonCommercial 4.0 International	*
dc.rights.uri	http://creativecommons.org/licenses/by-nc/4.0/	*
dc.subject	Combustible inertial LV	en_UK
dc.subject	Self-feeding rocket propulsion	en_UK
dc.title	Investigations of a combustible inertial launch design	en_UK
dc.type	Article	en_UK

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