No AccessTemperature Sensitivity of Composite Propellant Containing Novel Nano-Additive CatalystsAndrew R. Demko, James C. Thomas, Thomas Sammet, Eric L. Petersen, David Reid and Sudipta SealAndrew R. DemkoTexas A&M UniversitySearch for more papers by this author, James C. ThomasTexas A&M UniversitySearch for more papers by this author, Thomas SammetTexas A&M UniversitySearch for more papers by this author, Eric L. PetersenTexas A&M UniversitySearch for more papers by this author, David ReidUniversity of Central FloridaSearch for more papers by this author and Sudipta SealUniversity of Central FloridaSearch for more papers by this authorAIAA 2014-3691Session: Solid Rocket Motor Nozzles, Ignition Systems and PropellantsPublished Online:25 Jul 2014https://doi.org/10.2514/6.2014-3691SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byTemperature Sensitivity of AP/HTPB-Based Rocket Propellants Using a New High-Pressure Strand BurnerCatherine A. Dillier, Andrew Demko, Jacob Stahl, David Reid and Eric L. Petersen5 January 2017Aging Effects of Composite AP/HTPB Propellants Containing Nano-Sized AdditivesThomas Sammet, Andrew R. Demko, Catherine Dillier and Eric L. Petersen23 July 2015 What's Popular 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference July 28-30, 2014Cleveland, OHhttps://doi.org/10.2514/6.2014-3691 CrossmarkInformationCopyright © 2014 by The Authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsCatalysisChemical KineticsCombustion ChambersCooling TechnologyHeat ExchangersHeat TransferIgnition SystemsRocket EngineRocketryThermal EffectsThermal MeasurementThermochemistry and Chemical KineticsThermocouplesThermodynamic PropertiesThermodynamicsThermophysical PropertiesThermophysics and Heat Transfer KeywordsCatalystsHydroxyl Terminated PolybutadieneAluminized PropellantsSteady State CombustionThermal ConductivityElectrostatic DischargeHeat TransferData AcquisitionIgnition SystemsThermocouplesPDF Topics Solid Rockets