Theoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzle

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dc.AffiliationOctober University for modern sciences and Arts (MSA)
dc.contributor.authorEl-Nady, , AM
dc.contributor.authorSarhan, AM
dc.contributor.authorEl-Senbawy, , MA
dc.contributor.authorAhmed, , MYM
dc.date.accessioned2019-11-23T10:30:59Z
dc.date.available2019-11-23T10:30:59Z
dc.date.issued2017
dc.descriptionAccession Number: WOS:000395741800026en_US
dc.description.sponsorshipAMER INST AERONAUTICS ASTRONAUTICSen_US
dc.description.urihttps://www.scimagojr.com/journalsearch.php?q=29587&tip=sid&clean=0
dc.identifier.citationCited References in Web of Science Core Collection: 10en_US
dc.identifier.doihttps://doi.org/
dc.identifier.issn0748-4658
dc.identifier.otherhttps://doi.org/
dc.identifier.urihttps://cutt.ly/2eVueMZ
dc.language.isoenen_US
dc.publisherAMER INST AERONAUTICS ASTRONAUTICSen_US
dc.relation.ispartofseriesJOURNAL OF PROPULSION AND POWER;Volume: 33 Issue: 2 Pages: 531-536
dc.relation.urihttps://t.ly/OMngM
dc.subjectUniversity for Modern Sciences and Artsen_US
dc.titleTheoretical Analysis of Dual-Thrust Rocket Motors with Intermediate Nozzleen_US
dc.typeArticleen_US

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