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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 components for propulsion.

    Date

    2017-09-27

    Time

    09:45

    Room

    Hall E3

    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: Ms. Elizabeth Driscoll, Spaceflight, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: THE AEROJET ROCKETDYNE AR1 STAGED COMBUSTION BOOSTER ROCKET ENGINE

    25'

    Mr. Tom Martin

    Aerojet Rocketdyne

    United States

    2

    Ablation experimental characterization and numerical investigation of a 3-dimensionally built carbon/phenolic composite for aerospace applications

    13

    confirmed

    Mr. Michel BERDOYES

    Airbus Safran Launchers

    France

    3

    Plume Flow Field Analysis for Lander Propulsion System of Chandrayaan-2 Mission

    13

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    4

    Ceramic Catalyst Bed for a Green Liquid Bi-propellant Rocket Engine Using 98% Hydrogen Peroxide as Oxidizer

    13

    confirmed

    Dr. Pawel Surmacz

    Institute of Aviation

    Poland

    5

    optical spectroscopy on laser-induced ignition sparks and other space-relevant plasmas

    13

    withdrawn

    Dr. Robert Stützer

    DLR (German Aerospace Center)

    Germany

    6

    experimental investigation of 150n liquid oxygen-liquid methane attitude control engine

    13

    confirmed

    Dr. cheng cheng

    Shanghai Insitute of Space Propulsion

    China

    8

    Technology Development of an Electrically Driven Pump Fed Storable Liquid Bi-Propellant for a Mars Ascent Vehicle.

    13

    confirmed

    Mr. david vaughan

    NASA JPL

    United States

    9

    Trade-off Study and Thruster System Test of Reaction Control System for Reusable Rocket Boosters

    13'

    withdrawn

    Dr. Kiyoshi Kinefuchi

    JAXA

    Japan

    10

    Additive Manufacturing Development for Rocket Engine in Japan

    13

    confirmed

    Ms. Akane Nagasaki

    Mitsubishi Heavy Industries, Ltd.

    Japan

    11

    Test of flow deflector proof-of-concept models in LOX/Methane combustion gases.

    13

    confirmed

    Mr. Yoan Boué

    ArianeGroup SAS

    France

    12

    A Study on the Condensed Primary Combustion Products of Boron-based Fuel-rich Propellant

    13

    confirmed

    Dr. Wen Ao

    Northwestern Polytechnical University

    China

    13

    Comparative analysis regarding usage of different Reaction Control System on microlauncher attitude control

    13'

    withdrawn

    Prof. Teodor-Viorel Chelaru

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    14

    Green Options for Orbital Propulsion

    13'

    withdrawn

    Mr. Ulrich Gotzig

    Airbus Safran Launchers

    Germany