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  • session 3

    Title

    Propulsion Technology (1)

    type

    oral

    Description

    This session included all science and technologies supporting all aspects of space propulsion. The emphasis in this session is plased in particular components for propulsion.

    Date

    2015-10-14

    Time

    09:45

    Room

    Ballroom B (Crowne Plaza Hotel, -1 floor)

    IPC members
    • Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;

    • Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;

    • Rapporteur: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    jet inducer for a turbo pump of a liquid rocket engine

    15'

    confirmed

    Mr. Wolfgang Kitsche

    German Aerospace Center (DLR)

    Germany

    2

    Engine Control System for the Main Engine of the Reusable Sounding Rocket

    15'

    confirmed

    Mr. Takeshi Kai

    Mitsubishi Heavy Industries, Ltd.

    Japan

    3

    New horizons for SMA (Shape Memory Alloy) in Space Propulsion Applications

    15'

    confirmed

    Mr. OFER LIVNE

    Rafael Advanced Defense Systems Ltd.

    Israel

    4

    In flight achievements and follow-on for Cold Gas Micro Propulsion applied to S/C Fine Pointing and Attitude Control G.Noci A.Polli

    15'

    confirmed

    Dr. Giovanni Enrico Noci

    Selex ES

    Italy

    5

    Overview of NASA’s Green Propellant Infusion Mission and NASA Glenn Research Center’s Thruster Testing and Plume Diagnostics

    15'

    confirmed

    Mr. Timothy Smith

    NASA

    United States

    7

    rafael passivation valve for satellites propulsion system

    15'

    confirmed

    Mr. Michael Zaberchik

    Rafael Advanced Defense Systems Ltd.

    Israel

    8

    cold Gas Propulsion system for the samson nano satellites

    15'

    confirmed

    Mr. Michael Zaberchik

    Rafael Advanced Defense Systems Ltd.

    Israel

    9

    Assessment of various fuel additives for reliable hypergolic ignition with 98+ HTP

    15'

    confirmed

    Mr. Wojciech Florczuk

    Institute of Aviation

    Poland

    11

    numerical simulation study on combustion performance of low thrust LOX/methane rocket engine

    15'

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    14

    Dynamic Calculation Model for an Attitude Control System that uses Tilting Nozzles

    15'

    confirmed

    Mr. Adrian Danciu

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania