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Electrolytic Combustion in the Polyvinyl Alcohol Plus Hydroxylammonium Nitrate Solid Propellant

2017; American Institute of Aeronautics and Astronautics; Volume: 33; Issue: 6 Linguagem: Inglês

10.2514/1.b36450

1533-3876

James K. Baird, Joshua R. Lang, Andrew Hiatt, Robert A. Frederick,

Electrohydrodynamics and Fluid Dynamics

No AccessTechnical NoteElectrolytic Combustion in the Polyvinyl Alcohol Plus Hydroxylammonium Nitrate Solid PropellantJames K. Baird, Joshua R. Lang, Andrew T. Hiatt and Robert A. Frederick Jr.James K. BairdUniversity of Alabama in Huntsville, Huntsville, Alabama 35899, Joshua R. LangUniversity of Alabama in Huntsville, Huntsville, Alabama 35899, Andrew T. HiattUniversity of Alabama in Huntsville, Huntsville, Alabama 35899 and Robert A. Frederick Jr.University of Alabama in Huntsville, Huntsville, Alabama 35899Published Online:19 Jul 2017https://doi.org/10.2514/1.B36450SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Sawka W. and McPherson M., "Electrical Solid Propellants: A Safe, Micro to Macro Propulsion Technology," AIAA Paper 2013-4168, July 2013. 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TopicsCombustionElectric PowerEnergyEnergy ConsumptionEnergy EconomicsEnergy Forms, Production and ConversionEnergy ProductionMonopropellantsPropellantPropulsion and PowerRocket Propellant KeywordsElectric Solid PropellantElectrolytic CombustionHydroxylammonium NitratePolyvinyl AlcoholEnergy EfficiencyAtmospheric ConditionsElectric PowerAerospace EngineeringElectric PotentialOhmic HeatingAcknowledgmentsThe research presented in this Note was funded by a contract supplied by the Missile Defense Agency. The authors acknowledge Digital Solid State Propulsion for providing comments on cathode combustion.PDF Received26 August 2016Accepted8 May 2017Published online19 July 2017