STSEL Space Transportation Systems Engineering Laboratory

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INTRODUCTION

効率的で安全な宇宙への移動先進的な宇宙ミッションの実現には、物理現象の精確な理解とその影響を正確に考慮した設計が鍵を握り、私たちの研究室では、国内外の機関と連携し、理論・数値解析・実験に基づく多角的アプローチ最適化・機械学習といった最先端手法を融合し、将来型宇宙輸送システムに関する研究を行っています。特に、スクラムジェット・複合サイクルエンジン・電気推進といった先進的推進システム、月や火星への深宇宙探査・有人宇宙飛行・ランデブーといった挑戦的宇宙ミッションに焦点を当て、宇宙輸送技術の研究開発と物理現象の解明に取り組んでいます。

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FEATURES

NEWS

Journal
October 2021
Article on Fast estimation of internal flowfields in scramjet intakes via reduced-order modeling and machine learning published in Physics of Fluids first-authored by Dr Shuvayan Brahmachary
Conference
August 2021
Paper on Survey of Low-Energy Transfers to Lunar Libration Point Orbits with Targeted L1 Transits presented by Mr Foo Yang at 2021 AAS/AIAA Astrodynamics Specialist Conference
Journal
July 2021
Article on Miniaturization perspectives of electrostatic propulsion for small spacecraft platforms published in Progress in Aerospace Sciences in collaboration with RMIT University and University of Greifswald
Conference
July 2021
Paper on Prediction of Internal Flowfield in Scramjet Intakes via Deep Learning presented by Mr Chihiro Fujio at Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2021
Journal
June 2021
Article on Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor published in Acta Astronautica in collaboration with RMIT University
Journal
June 2021
Article on Multi-fidelity approach for global trajectory optimization using GPU-based highly parallel architecture published in Aerospace Science and Technology in collaboration with JAXA
Lab
April 2021
New Bachelor’s student members joined STSEL
Lab
April 2021
New Master’s student members joined STSEL
Journal
March 2021
Article on Physical Insight into Axisymmetric Scramjet Intake Design via Multi-Objective Design Optimization Using Surrogate-Assisted Evolutionary Algorithms published in Aerospace Science and Technology first-authored by Mr Chihiro Fujio
Journal
February 2021
Article on Numerical Investigation of Axisymmetric Intake Flowfield and Performance for Scramjet-Powered Ascent Flight published in Aerospace Science and Technology first-authored by Mr Chihiro Fujio