No AccessOn the Use of a Pulsed Nuclear Thermal Rocket for Interplanetary TravelFrancisco J. AriasFrancisco J. AriasUniversity of CataloniaSearch for more papers by this authorAIAA 2016-4685Session: Fusion and Alternative Nuclear Concepts IPublished Online:22 Jul 2016https://doi.org/10.2514/6.2016-4685SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byThrust Augmentation and its Control Methods: Short Overview1 December 2022 | REST Journal on Advances in Mechanical Engineering, Vol. 1, No. 4Heat Removal System for Shutdown in Nuclear Thermal Rockets and Advanced ConceptsFrancisco J. Arias and Geoffrey T. Parks9 February 2017 | Journal of Spacecraft and Rockets, Vol. 54, No. 4 What's Popular 52nd AIAA/SAE/ASEE Joint Propulsion Conference July 25-27, 2016Salt Lake City, UThttps://doi.org/10.2514/6.2016-4685 CrossmarkInformationCopyright © 2016 by Francisco Javier Arias Montenegro. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsCoolantCooling TechnologyHeat ConductionHeat TransferHeating, Ventilating, and Air ConditioningLaws of ThermodynamicsMass TransferThermodynamic PropertiesThermodynamicsThermophysical PropertiesThermophysics and Heat Transfer KeywordsPulsed Nuclear Thermal RocketPropellantCoolantRapid QuenchingFourier NumbersSecond Law of ThermodynamicsNuclear Pulse PropulsionThermohydraulicsHeat Transfer CoefficientsRocketsPDF Topics Nuclear and Future Flight Propulsion