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  • session 10

    Title

    Propulsion Technology (3)

    type

    oral

    Description

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

    Date

    2017-09-29

    Time

    11:00

    Room

    City Room 4

    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. Jerrol Littles, Aerojet Rocketdyne, United States;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Development of a Water Propulsion System for Small Satellites

    15

    confirmed

    Mr. Nicholas Harmansa

    IRS, University of Stuttgart

    Germany

    2

    Analysis of the pressure surge during fast transient in evacuated spacecraft feedlines

    15

    confirmed

    Mr. Cristiano Bombardieri

    DLR (German Aerospace Center)

    Germany

    3

    Numerical and Experiment Research of Nonsymmetric Cavitation Flow in Inducer During Head Drop

    15

    no-show

    Mr. Longxian Li

    Research & Development Center of China Academy of Launch Vehicle Technology

    China

    4

    Influence of Coaxial Injector on High-frequency Combustion Instability for Staged Combustion LOX/kerosene Rocket Engine

    15

    withdrawn

    Dr. Longfei Li

    Northwestern Polytechnical University

    China

    5

    The Experimental Investigation and On-orbit Flying Validation of an ADN-based Liquid Thruster

    15

    withdrawn

    Dr. Zhaopu Yao

    Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

    China

    6

    Catalyst Active Material Derivation for Ethanol-blended Hydrogen Peroxide Monopropellant Thruster

    15

    confirmed

    Mr. Seungkwan Baek

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    7

    Hypergolic Ionic Liquids as Green Propellants

    15

    confirmed

    Ms. Anna Thomas

    Stanford University

    United States

    8

    NEA Scout Propulsion System Testing

    15

    withdrawn

    Mr. Alber Douglawi

    Purdue University

    United States

    9

    Research on Thermal Decomposition of Hydrogen Peroxide For Low Thrust Propulsion System Application

    15

    confirmed

    Dr. Lukasz Mezyk

    Warsaw University of Technology (WUT)

    Poland

    10

    Characterization of Selective Laser Melting Impinging Injectors

    15'

    confirmed

    Mr. Deepak Atyam

    Purdue University

    United States

    11

    Advancement of Rocket Engine Performance through Novel Approaches for Thrust Chamber Design

    15

    confirmed

    Mr. Markus Ortelt

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    12

    Combustion dynamics in cryogenic rocket engines: research programme at DLR Lampoldshausen

    15

    confirmed

    Dr. Justin Hardi

    German Aerospace Center (DLR)

    Germany

    Characterization of Supercritical Properties in Atomization and Spray Characteristics of a Fuel Centred Pintle Injector in a 10kN Regenerative Cooled Pressure Fed Engine using Liquid Methane as Fuel

    15'

    withdrawn

    Mr. Rohan M Ganapathy

    Bellatrix Aerospace Private Limited

    India