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  • session 3

    Title

    Propulsion Technology (1)

    Description

    This session includes all science and technologies supporting all aspects of space propulsion. The emphasis in this session is placed, in particular, on components for propulsion.

    Date

    2018-10-03

    Time

    09:45

    Room

    ZARM 5

    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;

    • Rapporteur: Prof. Changjin Lee, Konkuk University, Korea, Republic of;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    09:45

    Carbon-carbon Nozzle Extension Assembly for the RL10 Engines

    13

    confirmed

    Mr. Thierry Pichon

    ArianeGroup

    France

    3

    09:58

    additive manufacturing development for le-9 engine

    13

    confirmed

    Mr. Akira Ogawara

    Mitsubishi Heavy Industries, Ltd.

    Japan

    4

    10:11

    Influences of structural parameters on atomization and combustion performances of LOX/methane pintle injector

    13

    confirmed

    Prof. Shen Chibing

    National University of Defense Technology

    China

    5

    10:24

    Development Status of Hydroxylammonium-Nitrate-Based Propulsion System with Discharge Plasma System

    13

    withdrawn

    Dr. Asato Wada

    Tokyo Metropolitan University

    Japan

    6

    10:37

    Hybrid Rockets with Nozzles in Ultra-High-Temperature Ceramic Composites

    13

    confirmed

    Mr. Giuseppe Di Martino

    University of Naples "Federico II"

    Italy

    7

    10:50

    Comparison of simulation and experimental results for functional verification of a propellant mass-flow regulation device

    13

    confirmed

    Dr. Samuel Webster

    ArianeGroup

    Germany

    8

    11:03

    Development and Qualification of Turbines for the Vinci Upper Stage Engine for Ariane 6

    13

    confirmed

    Ms. Li Forsberg

    GKN Aerospace Engine Systems

    Sweden

    9

    11:16

    Status of the Turbopump Development in the LUMEN Project

    13

    confirmed

    Mr. Tobias Traudt

    DLR (German Aerospace Center)

    Germany

    10

    11:29

    systems advantages of electric pump fed upper stage hybrid rocket

    13

    confirmed

    Mr. Kaan Gegeoglu

    Koc University

    Turkey

    11

    11:42

    Electrical Pressurization Concept for the Orion-ESM Propulsion System

    13

    confirmed

    Dr. Jan-Hendrik Meiss

    Airbus DS GmbH

    Germany

    12

    11:55

    Development Status of 500 N - class HTP/TMPDA Bi-propellant Rocket Engine

    13

    confirmed

    Dr. Pawel Surmacz

    Institute of Aviation

    Poland

    13

    12:08

    Development of 10N Mark-2 Thruster for Spacecraft Applications

    13

    confirmed

    Dr. ARUN KUMAR P

    Liquid Propulsion Systems Centre(LPSC), Indian Space Research Organization (ISRO)

    India

    14

    12:21

    Investigation of New Ignition Systems for Future Launcher Application

    13

    Dr. Laurent Gomet

    ArianeGroup

    France

    15

    12:34

    Modal Propellant Gauging: High-resolution and non-invasive gauging of both settled and unsettled liquids in reduced gravity.

    13

    confirmed

    Prof. Kevin Crosby

    Carthage College

    United States