Synthesis, characterization and application of  nanocomposites as burn rate modifiers in  solid composite propellant

dc.contributor.author	KUMAR, HARISH
dc.date.accessioned	2023-05-16T06:14:16Z
dc.date.available	2023-05-16T06:14:16Z
dc.date.issued	2017-08
dc.description	This Thesis submited by IIT BHU Varanasi Phd scholar and supervised by Prof. P K Mishra and P N Tengli	en_US
dc.description.abstract	Solid rocket motors are the simplest form of all rocket motors. The performance reliability, ease of operation, more safe in transportation and storability made them more attractive in propulsion industries. Theses mentioned unique properties of SRMs are due the solid composite propellant. The chemical composition of solid composite propellant can be tailored to meet the desired mission requirement i.e. mechanical and ballistic properties. These are few reasons due to which SRMs became famous for use in spite of having the less specific impulse over its counter part of liquid engines.	en_US
dc.identifier.other	TH503
dc.identifier.uri	https://idr-sdlib.iitbhu.ac.in/handle/123456789/2379
dc.language.iso	en	en_US
dc.publisher	iit bhu varanasi	en_US
dc.rights.license	CC BY-NC-SA 4.0
dc.subject	nanocomposites	en_US
dc.subject	solid composite propellant	en_US
dc.title	Synthesis, characterization and application of nanocomposites as burn rate modifiers in solid composite propellant	en_US
dc.type	Thesis	en_US