- 2018 - 2022 Investigation for Speed Ratio Dependence of Rarefied Aerodynamics Using Hypersonic Rarefied Wind Tunnel
- 2018 - 2021 Study of Ablative Thermal Protection System with Functionally Graded Materials
- 2017 - 2020 Accurate Prediction of Mars Entry Systems Hypersonic Aerodynamics with Strong Real Gas Effects Involved
- 2015 - 2018 Development of Measurement System for Martian Rarefied Aerodynamics and Investigation of Condensation Effect in Hypersonic Rarefied Wind Tunnel
- 2014 - 2017 Nonequilibrium Radiation Heating Acting on Atmospheric Entry Systems for Planets with CO2 Atmosphere
- 2012 - 2016 Development of Non-Ablative Lightweight Thermal Protection System for Planetary Exploration and Crew Space Transportation System
- 2012 - 2015 Developement of a hybrid ablation sensor
- 2012 - 2014 Development of an apparatus for catalytic coefficient measurement on thermal protection systems and construction of surface catalytic model
- 2010 - 2012 Radiation Coupled Complex Flow Field Modeling by Integration ofultrafast VUV spectroscopy and quantum chemical analysis
- 2010 - 2011 Prediction accuracy evaluation of analysis method for ablation thermal protection system using a general-purpose ablative materials
- 2009 - 2011 A measurement of the nonlinear thermomechanical characteristic and a development of a mathematical model for an ultra-lightweight carbon fiber reinforced plastic
- 2008 - 2009 High fidelity modeling of surface catalysis of materials toward improvement of evaluation method of thermal protection system
- 2006 - 2008 Improved Modeling of Nonequilibrium Thermochemistry by Advanced Optical Measurement and Microscopic State-to-state Analysis
- 2006 - 2007 アブレーション熱防御システムの高信頼設計手法の開発
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