Advanced and Combined Propulsion Systems
The session is for the presentation of advanced propulsion concepts being studied or considered. The advanced concepts should seek to deliver breakthroughs in overcoming the limitations of propulsion systems in current use or development. For advanced concepts technologies should normally be in the range TRL 0 to TRL 2. Advanced concepts with higher TRL technologies may also be presented where a combination of propulsion technologies can lead to performance breakthroughs which can not be achieved with a single technology. A combination can include for example both chemical and electric or solid and liquid chemical.
2012-10-05
Chairman: Mr. Jacques Gigou, European Space Agency (ESA), France;
Chairman: Mr. Richard Blott, British Interplanetary Society, United Kingdom;
Rapporteur: Mr. William W. Smith, Aerojet Rocketdyne, United States;
Order | Time | Paper title | Selection result | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|---|
1 | accepted | 15' | confirmed | Mr. Anirudh Thimmaiah | India | |||
2 | accepted | 15' | confirmed | Prof. igor Kurkin | Moscow Aviation Institute | Russian Federation | ||
3 | Application of the Continuous Rotating Detonation to Jet and Rocket Propulsion | accepted | 15' | confirmed | Prof. Piotr Wolanski | Polish Academy of Sciences | Poland | |
4 | Project Icarus: Analysis of Magnetic Nozzle Design for a Pulsed-Fusion Propulsion System | accepted | 15' | confirmed | Mr. Richard Hatcher | Propulsion Research Center, University of Alabama in Huntsville | United States | |
5 | Numerical study of tubular heat exchanger in the air-breathing engine with manifold | accepted | 15' | withdrawn | Mr. KIM SANGJO | Pusan National University | Korea, Republic of | |
6 | Design and Performance Study of A New Laser-electromagnetic Coupling Plasma Thruster | accepted | 15' | confirmed | Mr. Daixian Zhang | College of Aerospace Science and Engineering, National University of Defense Technology | China | |
7 | Developments of microwave rocket as a future low-cost mass transportation system | accepted | 15' | confirmed | Mr. Toshikazu Yamaguchi | The University of TOKYO, Graduate school | Japan | |
8 | Mixing enhancement in Hybrid rocket motor using vortex generators | accepted | 15' | confirmed | Prof. Fulvio Stella | Universita' di Roma 'La Sapienza' | Italy | |
9 | Pulsed Micro-thrust Measurement Using Torsional Pendulum Techniques | accepted | 15' | withdrawn | Mr. Daixian Zhang | College of Aerospace Science and Engineering, National University of Defense Technology | China | |
10 | Study of laser propulsion: one-dimensional modeling of Laser-Supported Detonation | accepted | 15' | confirmed | Mr. Toshikazu Yamaguchi | Japan | ||
11 | Two- and three-dimensional particle-in-cell simulation of magneto plasma sail | accepted | 15' | confirmed | Mr. yasumasa ashida | Research Institute for Sustainable Humanosphere, Kyoto University | Japan | |
12 | Numerical Investigation on Laser Ablation Characteristics of PTFE in Advanced Propulsion Systems | accepted | 15' | withdrawn | Mr. Daixian Zhang | College of Aerospace Science and Engineering, National University of Defense Technology | China |