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  • session 10

    Title

    Propulsion Technology (3)

    type

    oral

    Description

    This session includes all science and technologies supporting all aspects of space propulsion.

    Date

    2018-10-05

    Time

    13:30

    Room

    Bremen 3

    IPC members
    • Co-Chair: Mr. Norbert Puettmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

    • Co-Chair: Prof. Riheng Zheng, Beihang University, China;

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

    • Rapporteur: Mr. Martin Velander, GKN Aerospace Engine Systems, Sweden;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    13:30

    KEYNOTE: Green Solutions for Space Propulsion

    24

    confirmed

    Mr. Ulrich Gotzig

    ArianeGroup

    Germany

    2

    13:54

    Combustion Characterstics of Lox-Methane in Swirl Coaxial Injector Hydrogen Propulsion System

    13

    confirmed

    Dr. Sunil Kumar S.

    Indian Space Research Organization (ISRO)

    India

    3

    14:07

    Research on the key technology of the ‘swing behind pump’ thrust vector regulation architecture used in large thrust LOX/kerosene engine

    13

    confirmed

    Mr. Jian ZHAO

    Xi'an Aerospace Propulsion Institute

    China

    4

    14:20

    Maximizing side force generation in aerospike nozzles for attitude and trajectory control

    13

    confirmed

    Mr. Martin Propst

    TU Dresden

    Germany

    5

    14:33

    Cryo-Laboratory for the Investigation of Propellant Behaviour and Development of Propellant Management Technologies

    13

    confirmed

    Dr. Jens Gerstmann

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Institute of Space Systems

    Germany

    6

    14:46

    Numerical investigation on performance of fuel booster turbopump for staged combustion cycle based rocket engine.

    13

    confirmed

    Mr. KHALID RASHID

    Indian Space Research Organization (ISRO)

    India

    7

    14:59

    Hydraulic Development Testing of the Pressurization Concept for the Orion-ESM Propulsion System

    13

    withdrawn

    Dr. Jan-Hendrik Meiss

    Airbus DS GmbH

    Germany

    8

    15:12

    FLPP3: TEST RESULTS OF FULL ELECTRICALLY ACTUATED ENGINE VALVES

    13

    withdrawn

    Mr. Felipe Juan Dengra Moya

    ArianeGroup

    Germany

    9

    15:25

    Sloshing and Pressurization Tests for Membrane Tank: Tests, Validation and Models

    13

    confirmed

    Dr. Jörg Klatte

    ArianeGroup

    Germany

    10

    15:38

    Test of a highly reusable LOx/Methane gas generator demonstrator in a flight-like configuration

    13

    confirmed

    Dr. Sebastian Soller

    ArianeGroup

    Germany

    11

    15:51

    Identification and Maturation of Technologies for Future Liquid Propellant Engines

    13

    confirmed

    Dr. Sebastian Soller

    ArianeGroup

    Germany

    12

    16:04

    CFD simulation of reactive flow in cryogenic rocket nozzle and performance prediction of LVM III CE20 nozzle

    13

    confirmed

    Mr. Ajith M

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India

    13

    16:17

    The pyronumeric, a new technology to answer to the future launchers challenges

    13

    confirmed

    Mrs. Nathalie CESCO

    Centre National d'Etudes Spatiales (CNES)

    France