Please use this identifier to cite or link to this item: http://gukir.inflibnet.ac.in:8080/jspui/handle/123456789/4305
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dc.contributor.authorViswanath J.V
dc.contributor.authorVijayadarshan P
dc.contributor.authorMohan T
dc.contributor.authorRao N.V.S
dc.contributor.authorGupta A
dc.contributor.authorVenkataraman A.
dc.date.accessioned2020-06-12T15:03:01Z-
dc.date.available2020-06-12T15:03:01Z-
dc.date.issued2018
dc.identifier.citationJournal of Energetic Materials , Vol. 36 , 1 , p. 69 - 81en_US
dc.identifier.uri10.1080/07370652.2017.1313911
dc.identifier.urihttp://gukir.inflibnet.ac.in:8080/jspui/handle/123456789/4305-
dc.description.abstractPresent report emphasises the importance of employing a nano-copper chromite having an excess cupric oxide (CUCRO) as a ballistic modifier in a typical solid rocket propellant (SRP) composition. The CUCRO synthesised from a modified combustion route through decomposition of the alginate mixed metal complex is employed in the present investigation. The changes occurring in the mechanical properties of the propellant strands on addition of the CUCRO modifier are studied. Different morphologies are observed, which contribute towards the toughened propellant composition. The ballistic studies are undertaken in the presence and absence of CUCRO. © 2017 Taylor & Francis Group, LLC.en_US
dc.publisherTaylor and Francis Inc.
dc.subjectAlginate template route
dc.subjectballistic modifier
dc.subjectcopper chromite
dc.subjectspinel
dc.subjectthermal decomposition
dc.titleCopper Chromite as Ballistic Modifier in a Typical Solid Rocket Propellant Composition: A Novel Synthetic Route Involveden_US
dc.typeArticle
Appears in Collections:1. Journal Articles

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