IAF Digital Library

3

session 3

Title: Propulsion Technology
type: oral
Description: This session includes all science and technologies supporting all aspects of space propulsion. The emphasis in this session is plased in particular on components for propulsion.
Date: 2013-09-25
Time: 09:45
Room: 208A

IPC members

Chairman: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;
Chairman: Dr. George Schmidt, NASA Glenn Research Center, United States;
Rapporteur: Mr. Didier Boury, ArianeGroup SAS, France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Development and Testing of Nitrous Oxide/Propane Rocket Engine	15'	withdrawn	Dr. Wang Dong	Xi'an Aerospace Propulsion Institute	China
2		Development of Green Propellant Reaction Control System (GPRCS) for SERVIS-3 Project	15'	confirmed	Mr. Tetsuya Matsuo	Mitsubishi Heavy Industries, Ltd.	Japan
3		A novel kind of green high energy solid propellant containing hydrogen peroxide	15'	confirmed	Mr. Zhang Yungang		China
4		Recent progress on the development of a LOX/LCH4 rocket engine demonstrator in the framework of the Italian HYPROB program	15'	confirmed	Dr. Vito Salvatore	CIRA Italian Aerospace Research Center, Capua	Italy
5		Development of combustion technologies using the DLR P8 cryogenic test bench	15'	confirmed	Mr. Patrick Danous	Snecma	France
6		the development of high performance bipropellant rocket engine of small thrust class	15'	confirmed	Mr. Jian Li	Beijing Aerospace Propulsion Institute	China
7		self-pressurizing propellant tank dynamics	15'	confirmed	Mr. Jonah Zimmerman	Stanford University	United States
8		Cryogenic Propellant Tank Pressurisation Systems for Cryogenic Upper Stage of Geo Synchronous Satellite Launch Vehicle	15'		Mr. Sathis kumar B	Indian Space Research Organization (ISRO)	India
9		development and testing of a pistonless rocket engine pump technology demonstrator	15'	confirmed	Mr. Matthew Cannella	Colorado Center for Astrodynamics Research, University of Colorado	United States
10		Research and Development of the Turbopump for a Hydrogen Peroxide/Kerosene Rocket Engine with Staged Combustion Cycle	15'	confirmed	Dr. Hui CHEN	Xi'an Aerospace Propulsion Institute	China
11		slurry-propellant rocket propulsion. eco-safety and new power opportunities. tests of new propellants.	15'	confirmed	Mr. Yulian Protsan	The Laboratory of Advanced Jet Propulsion	Ukraine
12		a survey of the health monitoring technology for liquid-propellant rocket engines	15'	confirmed	Prof. Jianjun Wu	College of Aerospace Science and Engineering, National University of Defense Technology	China