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Future Throttle Valve

dc.contributor.authorAssenov, Ioan
dc.contributor.authorBeveridge, Noah
dc.contributor.authorHintzen, Michael
dc.contributor.authorVan Noord, Abigail
dc.contributor.advisorHyde
dc.date.accessioned2025-05-16T18:36:51Z
dc.date.available2025-05-16T18:36:51Z
dc.date.issued2025-05
dc.identifier.urihttps://hdl.handle.net/2027.42/197416
dc.description.abstractThe Michigan Aeronautical Science Association (MASA) has commissioned a group to design, build, and test a throttle valve that will be used in conjunction with other new technologies to give future rockets the ability to throttle their thrust, resulting in increased efficiency and altitude. The device must meet performance specifications required for integration with the full vehicle, safely operate with cryogenic liquid oxygen, allow for fairly deep throttle capabilities, be robust to a flight-like load environment, and be limited in mass such that there is a benefit to the new system architecture the valve is being designed to function in.
dc.description.sponsorshipMichigan Aeronautical Science Association (MASA)
dc.subjectValve
dc.subjectcryogenic
dc.subjectliquid rocketry
dc.subjectactive control
dc.subjectthrottle valve
dc.subjectME450en_US
dc.titleFuture Throttle Valve
dc.typeproject
dc.subject.hlbsecondlevelMechanical Engineering
dc.subject.hlbtoplevelEngineering
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/197416/1/MASA_Hyde_W25_T12_Future-Throttle-Valve.pdf
dc.identifier.doihttps://dx.doi.org/10.7302/25841
dc.working.doi10.7302/25841en
dc.owningcollnameMechanical Engineering, Department of


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