STSEL Space Transportation Systems Engineering Laboratory

NEWS

Conference
November 2022
Paper on Shape Optimization of Microwave Electrothermal Thruster Nozzle by Evolutionary Algorithms presented by Mr Keisuke Suenaga at The Japan Society for Aeronautical and Space Sciences Western Branch Symposium (日本航空宇宙学会西部支部講演会 2022)
Conference
September 2022
Paper on Multi-Objective Design Optimization of Scramjet Intakes via Evolutionary Algorithms Assisted by Multi-Dimensional Predictive Modeling Based on Deep Learning presented by Mr Chihiro Fujio at 2nd International Conference on High-Speed Vehicle Science and Technology (HiSST 2022)
Conference
May 2022
Paper on Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion presented by Mr Debdoot Ghosh at 26th AIAA Aerodynamic Decelerator Systems Technology Conference in Toulouse, France
Conference
March 2022
Paper on Multi-Objective Design Optimisation of Scramjet and Rocket Powered Launch Vehicle toward Fully Reusable Space Transportation System presented by Prof Hideaki Ogawa at 61st Conference on Aerospace Propulsion and Power (第61回航空原動機・宇宙推進講演会)
Conference
March 2022
Paper on Sensitivity Analysis of Fluid Behavior in Scramjet Intakes via Deep Learning Flow Prediction presented by Mr Chihiro Fujio at 61st Conference on Aerospace Propulsion and Power (第61回航空原動機・宇宙推進講演会)
Conference
March 2022
Paper on Optimization of Fuel Injection for Scramjet Engines based on Automatic Differential via Deep Learning presented by Mr Kento Akiyama at 61st Conference on Aerospace Propulsion and Power (第61回航空原動機・宇宙推進講演会)
Conference
March 2022
Paper on Fast Prediction and Sensitivity Study of Two-Dimensional Fuel Injection Flowfields via Deep Learning presented by Mr Kento Akiyama at 33rd ISTS (International Symposium on Space Technology and Science)
Conference
March 2022
Paper on Multi-Objective Design Optimization of Microwave Electrothermal Thruster presented by Mr Tsubasa Ozawa at 33rd ISTS (International Symposium on Space Technology and Science)
Conference
January 2022
Paper on Scramjet Intake Design Based on Exit Flow Profile via Global Optimization and Deep Learning toward Inverse Design presented by Mr Chihiro Fujio at AIAA Scitech 2022 Forum
Conference
November 2021
Paper on Multi-Point Forebody Shape Optimization for Reusable Launch System Using Rocket and Scramjet Propulsion presented by Mr Taiki Watanabe at The Japan Society for Aeronautical and Space Sciences Western Branch Symposium (日本航空宇宙学会西部支部講演会 2021)