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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

    2019-10-22

    Time

    09:45

    Room

    143A

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

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

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    KEYNOTE: Propulsion Technology Development Activities at NASA

    25

    Dr. George Schmidt

    NASA Glenn Research Center

    United States

    2

    10:10

    Feasibility Study on Electric Pumps Feeding Propellants to a Rocket Engine

    13

    confirmed

    Dr. MITSURU SHIMAGAKI

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    10:23

    Hot-Fire Test of the ETID Sandwich Nozzle Extension for Future Upper Stage Engine Applications

    13

    confirmed

    Mr. Klas Lindblad

    GKN Aerospace Engine Systems

    Sweden

    4

    10:36

    Channel Wall Nozzle Manufacturing Technology Advancements for Liquid Rocket Engines

    13

    confirmed

    Mr. Paul Gradl

    National Aeronautics and Space Administration (NASA)

    United States

    5

    10:49

    Progress in Additively Manufactured Copper-Alloy GRCop-84, GRCop-42, and Bimetallic Combustion Chambers for Liquid Rocket Engines

    13

    confirmed

    Mr. Paul Gradl

    National Aeronautics and Space Administration (NASA)

    United States

    6

    11:02

    The Development Process for a Single-Part Additively Manufactured Liquid Rocket Engine Injector with As-Printed Orifices

    13

    confirmed

    Mr. John Targonski

    University of Southern California

    United States

    7

    11:15

    Laser Metal Deposition Technology for LE-9 Engine

    13

    confirmed

    Mr. Akira Ogawara

    Mitsubishi Heavy Industries, Ltd.

    Japan

    8

    11:28

    Flame initiation inside the gas torch ignition system for a hybrid rocket motor

    13

    confirmed

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil

    9

    11:41

    LIQUID UPPER STAGE DEMONSTRATOR ENGINE (LUMEN): STATUS OF THE PROJECT

    13

    confirmed

    Mr. Tobias Traudt

    DLR (German Aerospace Center)

    Germany

    10

    11:54

    Developmental status of thruster in MHI (Mitsubishi Heavy Industries, Ltd.)

    13

    confirmed

    Mr. Daijiro Shiraiwa

    MHI

    Japan

    11

    12:07

    INTELLIGENT FLOW PROCESSING SYSTEM FOR HIGH THRUST ENGINES FOR MIXTURE RATIO CONTROL

    13

    confirmed

    Mr. elayaperumal ezhilrajan

    Indian Space Research Organization (ISRO)

    India

    12

    12:20

    Transient process simulation of 180kN LOX/Kerosene Upper Stage Engine with RocketEngine software version 2.0

    13

    confirmed

    Ms. Qun Liang

    Northwestern Polytechnical University

    China

    13

    12:33

    Open cell metal foam supported catalysts for hydrogen peroxide thrusters

    13

    confirmed

    Dr. Pawel Surmacz

    Institute of Aviation

    Poland