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  • session 3

    Title

    Propulsion Technology

    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