session 2
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
4 | Computational technology application for solid rocket motor burn simulation | 13 | withdrawn | Mr. Guilherme Mejia | Instituto Tecnológico de Aeronáutica (ITA) | Brazil | |
5 | design of a throttleable hybrid rocket propulsion platform for planetary soft landing | 13 | confirmed | Dr. Sheng Zhao | China Academy of Launch Vehicle Technology (CALT) | China | |
6 | 13 | withdrawn | Mr. Markus Jäger | Airbus Defence & Space, Space Systems | Germany | ||
7 | Simple Guidance Scheme for Low-Thrust Geostationary Orbit Transfers | 13 | Dr. Xue Ma | Beijing Institute of Control Engineering, China Academy of Space Technology (CAST) | China | ||
9 | Reusable Launch Vehicle-Concept of Minimizing Space Transportation Cost | 13 | withdrawn | Mr. Nadeem Alam | Department of Aeronautical Engineering, Babu Banarsi Das National Institute of Technology and Management, Lucknow, | India | |
12 | Thermodynamic Performance of 250kW Space Nuclear Power System Based on Liquid Metal Rankine Cycle | 13 | confirmed | Prof.Dr. Haochun Zhang | Harbin Institute of Technology | China | |
13 | Laser Ablation Propulsion Launch System (LAPLaS) Potentialities. | 13 | withdrawn | Mr. IOURI PIGULEVSKI | Switzerland | ||
16 | parametric analysis of a 30kN thrust class for nuclear thermal engine(nte)system | 13 | confirmed | Ms. Haoze Wang | Beijing Aerospace Propulsion Institute | China | |
17 | The studying of neutralizer characterization of multi-throttling point ion engine | 13 | withdrawn | Dr. yanhui jia | Lanzhou Institute of Physics | China | |
20 | 13 | confirmed | Mrs. Huiying Liu | State Key Laboratory of space power supply technology | China |