Thrust and Mixture Ratio Regulation Systems for Cryogenic Rocket Engines

dc.contributor.author	Narayan, V.
dc.date.accessioned	2015-01-30T07:25:22Z
dc.date.available	2015-01-30T07:25:22Z
dc.date.issued	1999-09
dc.identifier.govdoc	NB12768
dc.identifier.govdoc	NB12539
dc.identifier.uri	http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/3614
dc.language.iso	en	en
dc.publisher	IIT, Kharagpur	en
dc.subject	Mathematical Model	en
dc.subject	Cavitating Venturi	en
dc.subject	Engine Cycles	en
dc.subject	Engine Hot Tests	en
dc.subject	Mixture Ratio Regulation	en
dc.subject	Performance Analysis	en
dc.subject	Thrust Regulation	en
dc.subject	Algorithms for Engine Regulation	en
dc.subject	Cryogenic rocket engines	en
dc.subject	Mathematical Model	en
dc.title	Thrust and Mixture Ratio Regulation Systems for Cryogenic Rocket Engines	en
dc.type	Thesis	en