Design, Build and Test Small Scale Liquid Rocket Engine

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dc.contributor.authorMishra, Krishna Kant
dc.contributor.authorGautam, Prajwal
dc.contributor.authorYadav, Prakash
dc.date.accessioned2023-06-14T06:57:34Z
dc.date.available2023-06-14T06:57:34Z
dc.date.issued2023-03
dc.descriptionThe project entitled, “Design, Build and Test Small Scale Liquid Rocket Engine” reports about the liquid rocket engine which is a device in which liquid propellant is used to produce thrust. In this project at least 200N of thrust is aimed to be generated.en_US
dc.description.abstractThe project entitled, “Design, Build and Test Small Scale Liquid Rocket Engine” reports about the liquid rocket engine which is a device in which liquid propellant is used to produce thrust. In this project at least 200N of thrust is aimed to be generated. This project aims to generate thrust by using liquid propellant which is the combination of oxidizer and fuel. This project is an experimental study of the amount of thrust produced by the liquid rocket engine and design of various components needed to achieve the project target. The combustion chamber, nozzle, cylinder and fuel selection and design are focused and thus the target of the project is being achieved. This project helps us implement our knowledge and understanding of propulsion system and make us practically study its behavior which will surely be helpful for enhancing our knowledge and understanding of the propulsion phenomenon.en_US
dc.identifier.urihttps://hdl.handle.net/20.500.14540/17744
dc.language.isoenen_US
dc.publisherI.O.E. Pulchowk Campusen_US
dc.subjectDesign,en_US
dc.subjectBuild,en_US
dc.subjectRocketen_US
dc.titleDesign, Build and Test Small Scale Liquid Rocket Engineen_US
dc.typeReporten_US
local.academic.levelBacheloren_US
local.affiliatedinstitute.titlePulchowk Campusen_US
local.institute.titleInstitute of Engineeringen_US
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