IAF Digital Library

3

session 3

Title: Propulsion Technology
type: oral
Description: This session includes all science and technology supporting all aspects of space propulsion.
Date: 2008-10-01
Time: 09:30
Room: Dochart 2

IPC members

Chairman: Prof. Vladimir Prisniakov, Russian Academy of Sciences, Ukraine;
Chairman: Dr. Gennaro Russo, Campania Aerospace District, DAC, Italy;
Rapporteur: Mr. Alain Mercier, Snecma Propulsion Solide, France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Proven advanced technologies for space launcher SRM nozzles	presentation		Mr. Didier Boury	Herakles (Safran group)	France
2		Influence of external factors on starting and an operation of thermal pipes as a component of the space propulsion systems	presentation		Prof. Vladimir Prisniakov	Academy of Sciences	Ukraine
3		Cryogenic Thermal Design of Electromagnetic Formation Flight Satellites	presentation		Mr. Daniel Kwon	Massachusetts Institute of Technology (MIT)	United States
4		The Development of Japanese 20N Thruster Valve for a Spacecraft Propulsion System - Qualification test result -	presentation		Dr. Taiichi Nagata	Japan Aerospace Exploration Agency (JAXA)	Japan
5		feasibility study on nondestructive inspection for regenerative cooled combustion chamber by using neutron diffraction method and neutron radiography testing	presentation		Mr. Tadashi Masuoka	Japan Aerospace Exploration Agency (JAXA)	Japan
6		Experimental Investigation of the Evacuation Effect in Expansion Deflection Nozzles	presentation		Dr. Neil Taylor	University of Bristol	United Kingdom
7		Space propulsion components based on GAMMA TiAl BASED ALLOYS BY COMBUSTION SYNTHESIS+COMPACTION ROUTE	discussion		Mr. Jesus Marcos	INASMET-TECNALIA	Spain
8		Evaluation and Characterization of Laser Ignition Conditions for RCS Thruster Using Green Propellants	discussion		Dr. Shinichi Moriya	Japan Aerospace Exploration Agency (JAXA)	Japan
10		ROCKET NOZZLE DESIGN AND MANUFACTURE	discussion		Mr. Roland Rydén	Volvo Aero Corporation	Sweden
11		THE CALCULATION AND ANALYSIS OF FLEXIBLE JOINT ADHESION BONDED INTERFACE’S J-INTEGRAL IN SOLID ROCKET MOTOR	discussion		Mr. baolin sha		China
12		Pintle-controlled solid rocket motor research	discussion		Mr. yuan wu	Northwestern Polytechnical University	China
13		A New Method of Model-Based Diagnosis for Spacecraft Propulsion Systems	discussion		Mr. Wei Zheng	China Academy of Space Technology (CAST)	China
14		The DEIMOS III Engine Concept	discussion		Mr. Steven Engelen	Delft University of Technology (TU Delft)	The Netherlands
15		The improvement of the thrust and specific impulse by heating and elongating of de Laval nozzle	discussion		Mr. Yuuki IWAKI	Hokkaido University	Japan