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  • session 5

    Title

    Propulsion Technology (2)

    type

    oral

    Description

    This session includes all science and technologies supporting all aspects of space propulsion. An objective is to attract papers from students and young professionals with a more technical rather than programmatic or organisational focus.

    Date

    2017-09-28

    Time

    09:45

    Room

    Hall E3

    IPC members
    • Co-Chair: Mr. Walter Zinner, ArianeGroup, Germany;

    • Co-Chair: Mr. Jacques Gigou, European Space Agency (ESA), France;

    • Rapporteur: Mr. Zvika Zuckerman, Rafael Advanced Defense Systems Ltd., Israel;

    • Rapporteur: Mr. Max Calabro, The Inner Arch, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    KEYNOTE: The 1200kN-thrust-class LOX/Kerosene Rocket Engine for China New Generation Launch Vehicle

    30'

    withdrawn

    Dr. Hui CHEN

    Xi'an Aerospace Propulsion Institute

    China

    2

    10:15

    Modelling of Lunar Lander’s Thruster’s Exhaust Plume Impingement in Vacuum

    15

    no-show

    Mr. Mrigank Sahai

    India

    3

    10:30

    Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor

    15

    confirmed

    Mr. Wolfgang Armbruster

    German Aerospace Center (DLR)

    Germany

    4

    10:45

    Numerical Analysis of Combustion and Regenerative Cooling in LOX-Methane Rocket Engine

    15

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    5

    11:00

    Performance evaluation of water - hot gas ejector system used in liquid rocket engines

    15

    confirmed

    Dr. Ganesh Paramasivan

    ISRO Propulsion Complex, Mahendragiri, India

    India

    6

    11:15

    Optical Diagnostics for Characterization of Hypergolic Ignition in a Paraffin-Based Hybrid Rocket

    15

    withdrawn

    Mr. Keith Stober

    Stanford University

    United States

    7

    11:30

    Modeling and experimental validation for the passive Thermodynamic Vent System (TVS) of cryogenic propellant tank

    13

    confirmed

    Mr. JunHyuk Bae

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    8

    11:43

    Visco-plastic cyclic stress analysis of a semi-cryogenic engine thrust chamber

    15

    confirmed

    Mr. Krishnajith Jayamani

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

    India

    9

    11:58

    catalyst development and testing for ADN-fuel blends

    15

    confirmed

    Dr. Robert-Jan Koopmans

    Austria

    10

    12:13

    the flow characteristics study of floating ring seal of liquid rocket engine

    15

    withdrawn

    Mr. zhuang suguo

    Xi'an Aerospace Propulsion Institute

    China

    11

    12:28

    Effects of numerical simulation models on thermal characteristics of combustion gas flow ejected from gas oxygen/kerosene rocket engine

    15

    confirmed

    Dr. Junya Yuan

    Beihang University (BUAA)

    China

    12

    12:43

    Challenges in Realizing Instrumentation and Remote control systems for Testing Cryogenic Engine and stage

    15

    confirmed

    Mr. elayaperumal ezhilrajan

    Indian Space Research Organization (ISRO)

    India

    13

    12:58

    sensitivity analysis of static parameters for the lox/kerosene rocket engine

    15

    confirmed

    Dr. haohai xu

    School of Astronautics,Northwestern Polytechnical University

    China

    14

    13:13

    Periodic atomization of impinging injectors modulated by back pressure fluctuations

    15

    withdrawn

    Dr. Anlong Yang

    Xi'an Aerospace Propulsion Institute

    China