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  4. Thrust and Mixture Ratio Regulation Systems for Cryogenic Rocket Engines
Please use this identifier to cite or link to this item: http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/3614
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dc.contributor.authorNarayan, V.
dc.date.accessioned2015-01-30T07:25:22Z
dc.date.available2015-01-30T07:25:22Z
dc.date.issued1999-09
dc.identifier.govdocNB12768
dc.identifier.govdocNB12539
dc.identifier.urihttp://www.idr.iitkgp.ac.in/xmlui/handle/123456789/3614
dc.language.isoenen
dc.publisherIIT, Kharagpuren
dc.subjectMathematical Modelen
dc.subjectCavitating Venturien
dc.subjectEngine Cyclesen
dc.subjectEngine Hot Testsen
dc.subjectMixture Ratio Regulationen
dc.subjectPerformance Analysisen
dc.subjectThrust Regulationen
dc.subjectAlgorithms for Engine Regulationen
dc.subjectCryogenic rocket enginesen
dc.subjectMathematical Modelen
dc.titleThrust and Mixture Ratio Regulation Systems for Cryogenic Rocket Enginesen
dc.typeThesisen
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