session 1
- Title
Propulsion System (1)
- type
oral
- Description
This session is dedicated to all aspects of Liquid Rocket Engines.
- Date
2017-09-25
- Time
- Room
- IPC members
Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Co-Chair: Mr. Patrick Danous, ArianeGroup, France;
Rapporteur: Dr. Vanniyaperumal Narayanan, Indian Space Research Organization (ISRO), India;
Rapporteur: Mr. Akira Ogawara, Mitsubishi Heavy Industries, Ltd., Japan;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | KEYNOTE: Development Status of the Cryogenic Oxygen/Hydrogen YF -77 Engine for Long-March 5 | 30' | confirmed | Mr. Dayong Zheng | Beijing Aerospace Propulsion Institute | China | |
2 | 15' | confirmed | Mr. Christophe Bonhomme | Centre National d'Etudes Spatiales (CNES) | France | ||
3 | progress summary of engineering model firing tests in le-9 engine development | 15' | confirmed | Mr. Masaki Adachi | Mitsubishi Heavy Industries, Ltd. | Japan | |
4 | Design and Development Status of LE-9 Engine for H3 Launch Vehicle | 15 | confirmed | Mr. Akihide Kurosu | Japan Aerospace Exploration Agency (JAXA) | Japan | |
5 | 15' | confirmed | Mr. Tobias Traudt | DLR (German Aerospace Center) | Germany | ||
6 | Development Status of the 7tonf LOx/Kerosene Gas Generator Cycle Engine for KSLV-II | 15' | confirmed | Dr. CHANG HO NAM | Korea Aerospace Research Institute (KARI) | Korea, Republic of | |
7 | vinci engine thermo-structural composite nozzle extension for ariane 6 | 15' | confirmed | Mr. Herve COPERET | Airbus Safran Launchers | France | |
8 | Ignition of ADN-based monopropellants – Results of the european project RHEFORM | 15' | confirmed | Mr. Christian Hendrich | DLR (German Aerospace Center) | Germany | |
9 | 15' | confirmed | Mr. Oleg Safin | JSC NPO Energomash | Russian Federation | ||
10 | 15' | withdrawn | Mr. Patrick Danous | Airbus Safran Launchers | France | ||
10 | Continued Development of the Aerojet Rocketdyne AR1 Staged Combustion Booster Rocket Engine | 15 | confirmed | Mr. Tom Martin | Aerojet Rocketdyne | United States | |
11 | Orion European Service Module Propulsion Subsystem on Fire during Qualification Testing | 15' | confirmed | Mr. Markus Jäger | Airbus Defence & Space, Space Systems | Germany | |
12 | failure detection of liquid propellant rocket engine using system invariant analysis technology | 15' | confirmed | Dr. Masaki Sato | Japan Aerospace Exploration Agency (JAXA) | Japan | |
13 | AN ADDITIVELY-MANUFACTURED CNG/GOX AEROSPIKE ROCKET ENGINE: DESIGN PROCESS | 15' | confirmed | Mr. Graham Bell | Monash University | Australia |