session 1

Title: Propulsion System (1)
Description: This session is dedicated to all aspects of Liquid Rocket Engines.
Date: 2013-09-23
Time: 15:15
Room: 208A

IPC members

Chairman: Mr. Max Calabro, The Inner Arch, France;
Chairman: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Rapporteur: Mr. Walter Zinner, ArianeGroup, Germany;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		The Development of LOX/LH2 Engine in China	accepted	15'	confirmed	Mr. Nan Zhang	Beijing Aerospace Propulsion Institute	China
2		Development Status of the Cryogenic Oxygen/Hydrogen YF-77 Engine for Long-March 5	accepted	15'	confirmed	Mr. Weibin Wang		China
3		The VINCI upper stage engine: the demonstration of maturity	accepted	15'	confirmed	Mr. Patrick Danous	Snecma	France
4		technology demonstration status of le-x engine	accepted	15'	confirmed	Mr. Hideo Sunakawa	Japan Aerospace Exploration Agency (JAXA)	Japan
5		Cyclone-4 Launch Vehicle III stage engine. Ground testing results	accepted	15'		Mr. Alexandr Prokopchuk	Yuzhnoye State Design Office	Ukraine
6		Expand of Capabilities of Rocket and Space Complexes with High–Molecular Additives to Liquid Propellant Components	accepted	15'	confirmed	Dr. Valeriy Gaponov	JSC NPO Energomash	Russian Federation
7		Development and Test of the LOX/Methane Regenerative Cooled Rocket Engine (2nd Report)	accepted	15'	confirmed	Mr. Kohei Taya	IHI Corporation	Japan
8		Technological Demonstration Tests of main Engine for Reusable Sounding Rocket	accepted	15'	confirmed	Dr. Tomoyuki Hashimoto	Japan Aerospace Exploration Agency (JAXA)	Japan
9		System analysis and applied study in the field of a choice of rocket engines for perspective reusable launchers.	accepted	15'	confirmed	Mr. Yuri Gusev	TSNIIMASH	Russian Federation
10		Overview on Liquid Propulsion System Modeling Tools for Quick-Loop, Engineering and Design Studies	accepted	15'	confirmed	Mr. Markus Jäger	Astrium Space Transportation	Germany
11		Propulsion Control System Model for Liquid Rocket Engines Using Intelligent Techniques	accepted	15'		Mr. elayaperumal ezhilrajan	Indian Space Research Organization (ISRO)	India
12		Performance Analyses for Propulsion System of CE-2 Satellite with the Extra Missions	accepted	15'	confirmed	Mr. Liang Junqiang	Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)	China