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Combustion of HAN-based liquid monopropellants near the thermodynamic critical point

dc.contributor.authorKounalakis, M. E.en_US
dc.contributor.authorFaeth, Gerard M.en_US
dc.date.accessioned2006-04-07T20:09:07Z
dc.date.available2006-04-07T20:09:07Z
dc.date.issued1988-11en_US
dc.identifier.citationKounalakis, M. E., Faeth, G. M. (1988/11)."Combustion of HAN-based liquid monopropellants near the thermodynamic critical point." Combustion and Flame 74(2): 179-192. <http://hdl.handle.net/2027.42/27077>en_US
dc.identifier.urihttp://www.sciencedirect.com/science/article/B6V2B-497S7WB-96/2/c284f332b28e476fc75589dabfc33373en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/27077
dc.description.abstractThe high-pressure combustion properties of liquid monopropellants involving mixtures of hydroxyl ammonium nitrate (HAN), triethanol ammonium nitrate (TEAN), and water are considered theoretically. Liquid surface properties and the critical combustion pressure (the pressure required for the propellant surface to exceed its thermodynamic critical point) were found allowing for real-gas phenomena and the presence of dissolved combustion product gases in the liquid. Critical combustion pressures for the HAN-based monopropellants were found to be unusually high, ca. 2500 atm, with an estimated uncertainty of 50%. Predictions were unusually sensitive to the critical temperature of TEAN and the binary interaction parameter between TEAN and water; both must be known more accurately for definitive estimates of the liquid-surface properties of HAN-based monopropellants at high pressures.en_US
dc.format.extent998560 bytes
dc.format.extent3118 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.language.isoen_US
dc.publisherElsevieren_US
dc.titleCombustion of HAN-based liquid monopropellants near the thermodynamic critical pointen_US
dc.typeArticleen_US
dc.rights.robotsIndexNoFollowen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbsecondlevelMathematicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, The University of Michigan, Ann Arbor, MI 48109-2140, USAen_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, The University of Michigan, Ann Arbor, MI 48109-2140, USAen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/27077/1/0000068.pdfen_US
dc.identifier.doihttp://dx.doi.org/10.1016/0010-2180(88)90016-8en_US
dc.identifier.sourceCombustion and Flameen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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