STSEL Space Transportation Systems Engineering Laboratory

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INTRODUCTION

We aim to realise future space transportation systems for reliable and economical access-to-space and advanced space missions by thoroughly understanding physical phenomena and employing state-of-the-art design and optimisation methodologies in multidisciplinary and system engineering approaches. Our key focus areas include space transportation using advanced propulsion technologies, e.g., scramjet propulsion, combined cycle engines, electric propulsion systems, as well as challenging space missions including deep-space (lunar, interplanetary) missions, human space travel and rendezvous missions.

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FEATURES

NEWS

Lab
October 2022
Dr Suk Hyun Yeo appointed as Assistant Professor at STSEL
Journal
October 2022
Article on Deep-learning prediction and uncertainty quantification for scramjet intake flowfields published in Aerospace Science and Technology first-authored by Mr Chihiro Fujio
Journal
October 2022
Article on Nozzle design optimization for supersonic wind tunnel by using surrogate-assisted evolutionary algorithms published in Aerospace Science and Technology first-authored by Mr Masanobu Matsunaga
Journal
September 2022
Article on Multi-Objective Design Optimization of Cusped Field Thruster via Surrogate-Assisted Evolutionary Algorithms published in Journal of Propulsion and Power first-authored by Dr Suk Hyun Yeo
Lab
May 2022
Research student (Aric Bandera) arrived to join STSEL
Lab
April 2022
New Bachelor’s student members joined STSEL
Lab
April 2022
New Master’s student members joined STSEL
Journal
April 2022
Article on Improved modeling for design optimization of cusped field thrusters with support of kinetic analysis published in Acta Astronautica first-authored by Mr Suk Hyun Yeo
Journal
March 2022
Article on Design optimization and off-design performance analysis of axisymmetric scramjet intakes for ascent flight published in Physics of Fluids first-authored by Dr Shuvayan Brahmachary
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)