Development of Temperature Measurement Technique Using a Dual-Component Ablation Sensor

No AccessTechnical NoteDevelopment of Temperature Measurement Technique Using a Dual-Component Ablation SensorYuuki Dantsuka, Takeharu Sakai, Yuichi Ishida, Toshiyuki Suzuki and Kazuhisa FujitaYuuki DantsukaNagoya University, Nagoya 464-8603, Japan*Graduate Student, Department of Aerospace Engineering.Search for more papers by this author, Takeharu SakaiTottori University, Tottori 680-8550, Japan†Department of Mechanical and Aerospace Engineering; . Senior Member AIAA (Corresponding Author).Search for more papers by this author, Yuichi IshidaJapan Aerospace Exploration Agency, Tokyo 182-0012, Japan‡Associate Senior Researcher, Aeronautical Technology Directorate.Search for more papers by this author, Toshiyuki SuzukiJapan Aerospace Exploration Agency, Tokyo 182-0012, Japan§Associate Senior Researcher, Research and Development Directorate. Senior Member AIAA.Search for more papers by this author and Kazuhisa FujitaJapan Aerospace Exploration Agency, Tokyo 182-0012, Japan¶Manager for Space Exploration Technology, Research and Development Directorate. Senior Member AIAA.Search for more papers by this authorPublished Online:20 Nov 2017https://doi.org/10.2514/1.T5254SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Sakai T., Nakazawa H., Dantsuka Y., Ishida Y., Kitagawa K. and Hirai K., “Dual-Component Sensor Design for In-Situ Ablation Measurement,” Journal of Thermophysics and Heat Transfer, Vol. 31, No. 2, 2017, pp. 307–317. doi:https://doi.org/10.2514/1.T4843 JTHTEO 0887-8722 LinkGoogle Scholar[2] Muller B. and Renz U., “Development of a Fast Fiber-Optic Two-Color Pyrometer for the Temperature Measurement of Surfaces with Varying Emissivities,” Review of Scientific Instruments, Vol. 72, No. 8, 2001, pp. 3366–3374. doi:https://doi.org/10.1063/1.1384448 RSINAK 0034-6748 CrossrefGoogle Scholar[3] Wilson R. G. and Spitzer C. R., “Visible and Near-Infrared Emittance of Ablation Chars and Carbon,” AIAA Journal, Vol. 6, No. 4, 1968, pp. 665–671. doi:https://doi.org/10.2514/3.4560 AIAJAH 0001-1452 LinkGoogle Scholar[4] Fujita K., Suzuki T., Ozawa T., Sakai T., Dantsuka T., Ishida Y. and Watanabe Y., “Ablation Sensor Unit for Flight Demonstration on HTV Small Recovery Capsule,” AIAA Paper 2017-0899, Jan. 2017. LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byUnsteady Testing of an Ablation Sensor in Torch FlameTRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, Vol. 19, No. 4Review of Sensing Techniques of Ablative MaterialsChristine Yang and Joseph H. Koo5 January 2020Radiative Transfer in a Low-Density Ablative Material Under Arcjet Flow ConditionsBernard O. Owiti, Takeharu Sakai and Yuichi Ishida20 October 2019 | Journal of Thermophysics and Heat Transfer, Vol. 34, No. 1 What's Popular Volume 32, Number 3July 2018 CrossmarkInformationCopyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0887-8722 (print) or 1533-6808 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAblationAerodynamicsAeronautical EngineeringAeronauticsAerothermodynamicsAvionicsDiodesGuidance, Navigation, and Control SystemsSemiconductor DevicesSemiconductor DiodesSensorsThermal Control and ProtectionThermal MeasurementThermochemistry and Chemical KineticsThermodynamic PropertiesThermodynamicsThermometersThermophysics and Heat TransferTransducersWind Tunnels KeywordsAblation SensorsPhotodiodesRadiation ThermometryAblative MaterialsAblation Sensor UnitEmissivityWind TunnelsJapan Aerospace Exploration AgencyAerospace EngineeringSpace Exploration and TechnologyAcknowledgmentsThis research was supported by the Japan Society for Promotion of Science as Grant-in-Aid for Challenging Exploratory Research (No. 15K14251). The authors would like to thank Hirofumi Nakazawa and Kenta Iwamoto for their support during ablation sensor measurements, and the staff of the Wind Tunnel Technology Center of the Japan Aerospace Exploration Agency for their support during arcjet testing.PDF Received27 April 2017Accepted20 October 2017Published online20 November 2017