No AccessThermal and mechanical design of the MAIUS atom interferometer sounding rocket payloadJens Grosse, Stephan T. Seidel, Markus Krutzik, Marco Scharringhausen and Tim van ZoestJens GrosseGerman Aerospace Center (DLR)Search for more papers by this author, Stephan T. SeidelLeibniz University of HannoverSearch for more papers by this author, Markus KrutzikHumboldt University of BerlinSearch for more papers by this author, Marco ScharringhausenGerman Aerospace Center (DLR)Search for more papers by this author and Tim van ZoestGerman Aerospace Center (DLR)Search for more papers by this authorAIAA 2014-4210Session: Space Systems DevelopmentPublished Online:1 Aug 2014https://doi.org/10.2514/6.2014-4210SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byMicrogravity Test Complex for Mobile and Portable Optical Frequency Standards5 September 2022 | Measurement Techniques, Vol. 65, No. 3Quantum physics in space1 Mar 2022 | Physics Reports, Vol. 951JOKARUS - design of a compact optical iodine frequency reference for a sounding rocket mission22 May 2017 | EPJ Quantum Technology, Vol. 4, No. 1A compact and robust diode laser system for atom interferometry on a sounding rocket25 July 2016 | Applied Physics B, Vol. 122, No. 8 What's Popular AIAA SPACE 2014 Conference and Exposition 4-7 August 2014San Diego, CAhttps://doi.org/10.2514/6.2014-4210 CrossmarkInformationCopyright © 2014 by German Aerospace Center. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsConvectionCooling TechnologyHeat ConductionHeat ExchangersHeat PipesHeat TransferThermal Control and ProtectionThermodynamic PropertiesThermodynamicsThermophysics and Heat Transfer KeywordsSounding RocketsHeat SinksVibration IsolationEvaporative CoolingMagnetic ShieldingPower DistributionCritical TemperatureAttitude Control SystemFluorescencePhotodiodesDigital Topics Space Systems