session 3
- Title
Propulsion Technology (1)
- type
oral
- Description
This session includes all science and technologies supporting all aspects of space propulsion. The emphasis in this session is placed, in particular, on components for propulsion.
- Date
2019-10-22
- Time
- Room
- IPC members
Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Rapporteur: Prof. Changjin Lee, Konkuk University, Korea, Republic of;
Rapporteur: Mr. Martin Velander, GKN Aerospace Engine Systems, Sweden;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 09:45 | KEYNOTE: Propulsion Technology Development Activities at NASA | 25 | withdrawn | Dr. George Schmidt | NASA Glenn Research Center | United States |
2 | 10:10 | Feasibility Study on Electric Pumps Feeding Propellants to a Rocket Engine | 13 | confirmed | Dr. MITSURU SHIMAGAKI | Japan Aerospace Exploration Agency (JAXA) | Japan |
3 | 10:23 | Hot-Fire Test of the ETID Sandwich Nozzle Extension for Future Upper Stage Engine Applications | 13 | confirmed | Mr. Klas Lindblad | GKN Aerospace Engine Systems | Sweden |
4 | 10:36 | Channel Wall Nozzle Manufacturing Technology Advancements for Liquid Rocket Engines | 13 | confirmed | Mr. Paul Gradl | National Aeronautics and Space Administration (NASA) | United States |
5 | 10:49 | 13 | confirmed | Mr. Paul Gradl | National Aeronautics and Space Administration (NASA) | United States | |
6 | 11:02 | 13 | withdrawn | Mr. John Targonski | University of Southern California | United States | |
7 | 11:15 | 13 | confirmed | Mr. Akira Ogawara | Mitsubishi Heavy Industries, Ltd. | Japan | |
8 | 11:28 | Flame initiation inside the gas torch ignition system for a hybrid rocket motor | 13 | confirmed | Dr. Olexiy Shynkarenko | University of Brasilia | Brazil |
9 | 11:41 | LIQUID UPPER STAGE DEMONSTRATOR ENGINE (LUMEN): STATUS OF THE PROJECT | 13 | confirmed | Mr. Tobias Traudt | DLR (German Aerospace Center) | Germany |
10 | 11:54 | Developmental status of thruster in MHI (Mitsubishi Heavy Industries, Ltd.) | 13 | confirmed | Mr. Daijiro Shiraiwa | MHI | Japan |
11 | 12:07 | INTELLIGENT FLOW PROCESSING SYSTEM FOR HIGH THRUST ENGINES FOR MIXTURE RATIO CONTROL | 13 | withdrawn | Mr. elayaperumal ezhilrajan | Indian Space Research Organization (ISRO) | India |
12 | 12:20 | 13 | confirmed | Mrs. Lili Ren | National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an, | China | |
13 | 12:33 | Open cell metal foam supported catalysts for hydrogen peroxide thrusters | 13 | confirmed | Dr. Pawel Surmacz | Institute of Aviation | Poland |
* | Numerical investigation of rotating stall in high pressure fuel pump of semicryogenic engine | Mr. KHALID RASHID | Indian Space Research Organization (ISRO) | India |