session 1

Title: Propulsion System (1)
Description: This session is dedicated to all aspects of Liquid Rocket Engines.
Date: 2014-09-29
Time: 15:15
Room: 714B

IPC members

Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Co-Chair: Mr. Walter Zinner, ArianeGroup, Germany;
Rapporteur: Dr. Vanniyaperumal Narayanan, Indian Space Research Organization (ISRO), India;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		LOx/Methane Re-usable Propulsion System Development with implementation of Concurrent Engineering	accepted	15'	confirmed	Mr. Paul Valton	Airbus Defence and Space - Space Systems	France
2		NASA Space Launch System Advanced Booster Risk Reduction Status Report	accepted	15'	confirmed	Mr. Steve Cook	Dynetics	United States
3		Technology Demonstration Results of LE-X Engine	accepted	15'	withdrawn	Mr. Shusuke Hori	Japan Aerospace Exploration Agency (JAXA)	Japan
4		numerical simulation of a lo2-ch4 rocket engine demonstrator	accepted	15'	confirmed	Mr. Daniele Cardillo	CIRA Italian Aerospace Research Center, Capua	Italy
5		Development status of a 200 kN thrust Cryogenic upper stage engine for ISRO’s next generation launch vehicle	accepted	15'	confirmed	Dr. Vanniyaperumal Narayanan	Indian Space Research Organization (ISRO)	India
6		Flight testing of Indian Cryogenic Upper Stage	accepted	15'	confirmed	Dr. Vanniyaperumal Narayanan	Indian Space Research Organization (ISRO)	India
7		The Future of Cryogenic Propulsion	accepted	15'	confirmed	Mr. Christophe Bonhomme	Centre National d'Etudes Spatiales (CNES)	France
8		Modernization of powerful LOX-kerosene LPRE of NPO Energomash by change of fuel «kerosene» on «methane»	accepted	15'	confirmed	Mr. Vladimir Sudakov	JSC NPO Energomash	Russian Federation
9		modeling study on natural circulation precooling for cryogenic liquid rocket propulsion system	accepted	15'	withdrawn	Mr. Shiqiang Chen	China Academy of Launch Vehicle Technology, China	China
10		Design and Demonstration Tests of LOX/LH2 Engine for Reusable Sounding Rocket	accepted	15'	confirmed	Mr. Yuya FUKUDA	Mitsubishi Heavy Industries Ltd. Japan	Japan
11		student design/build/test of a throttleable lox-lch4 thrust chamber	accepted	15'	confirmed	Mr. Michael Bedard	Purdue University	United States
12		The VINCI propulsion system : new steps toward qualification	accepted	15'	confirmed	Mr. Patrick Danous	Snecma	France