• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-19
  • C4
  • 5
  • session 5

    Title

    Propulsion Technology (2)

    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

    2019-10-22

    Time

    14:45

    Room

    143A

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

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

    • Rapporteur: Mr. Jerome Breteau, European Space Agency (ESA), France;

    • Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    Aerodynamic Interactions of Ion Thruster Plume Plasmas in Very Low Earth Orbit

    13

    confirmed

    Mr. Shaun Andrews

    University of Bristol

    United Kingdom

    2

    14:58

    Robust Transient Control of Reusable Liquid-Propellant Rocket Engines

    13

    confirmed

    Mr. Sergio Pérez-Roca

    Centre National d'Etudes Spatiales (CNES)

    France

    3

    15:11

    novel propellant feed system for chemical in-space propulsion

    13

    withdrawn

    Mr. RITVIK PAREEK

    SRM University Chennai

    India

    4

    15:24

    Development and Qualification of a High Performance Solid Strapon Motor

    13

    no-show

    Mr. Mahesh V

    India

    5

    15:37

    computational study of aerospike engines for reusable rocket systems

    13

    withdrawn

    Mr. Sahil Bhatia

    University of Petroleum and Energy Studies

    India

    6

    15:50

    Implementation of Additive Manufacturing for the Design & Development of the Jessie & James Liquid Rocket Engines

    13

    withdrawn

    Mr. John Targonski

    University of Southern California

    United States

    7

    16:03

    Ultra-High-Temperature Ceramic Matrix Composites for Hybrid Rocket Nozzles

    13

    confirmed

    Mr. Stefano Mungiguerra

    Università degli Studi di Napoli “Federico II”

    Italy

    8

    16:16

    Updates on the Development of a Water Electrolysis Propulsion System

    13

    confirmed

    Mr. Nicholas Harmansa

    Institute of Space Systems, University of Stuttgart

    Germany

    9

    16:29

    Investigation on the Consequences of Employing Dual Throat Micronozzle in Microsatellite Propulsion

    13

    confirmed

    Mr. Raj Kedia

    R.V.College of Engineering

    India

    10

    16:42

    A newly developed high performance ADN based monopropellant with a safety evaluation

    13

    confirmed

    Mr. Ju Won Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    11

    16:55

    experimental study of ablation characteristics of hafnium-based composites in the hybrid rocket nozzle

    13

    confirmed

    Mr. Kyu-Seop Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    12

    17:08

    Numerical Simulation and Experimental Study on the Atomization Characteristics of Impinging Liquid Jets Coupled with Forced Perturbation

    13

    withdrawn

    Ms. Qun Liang

    Northwestern Polytechnical University

    China

    *

    Autophage Caseless Throttleable Solid Motor for Small Satellites

    withdrawn

    Dr. Patrick Harkness

    School of Engineering, University of Glasgow

    United Kingdom

    *

    Conjugated Heat Transfer Measurements with Methane in Rocket Nozzle Cooling Channels

    Dr. Jens Fridh

    Royal Institute of Technology (KTH)

    Sweden

    *

    Experimental and Numerical Chemical Kinetics Investigation of Nitrous Oxide Fuel Blends with Special Emphasis on Space Vehicle Contaminants

    withdrawn

    Mr. Martin Hoener

    University Duisburg-Essen

    Germany

    *

    STUDENT TEAM DEVELOPMENT OF BIPROPELLANT ELECTRIC FEED SYSTEM FOR 2.2kN ISOPROPYL ALCOHOL/LIQUID OXYGEN ROCKET ENGINE

    Mr. Julio Garcia

    Portland State Aerospace Society

    United States