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  • session 3

    Title

    Propulsion Technology

    type

    oral

    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

    2012-10-03

    Time

    10:15

    Room

    TS14 (Sala Capri, Palacongressi)

    IPC members
    • Chairman: Mr. John Harlow, Aerojet Rocketdyne, United Kingdom;

    • Chairman: Mr. James Free, National Aeronautics and Space Administration (NASA), United States;

    • Rapporteur: Mr. Didier Boury, ArianeGroup SAS, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Secondary injection thrust vectoring of an axisymmetric CD nozzle for small space launchers & vehicles

    15'

    confirmed

    Mr. Vladeta Zmijanovic

    ICARE-CNRS

    France

    2

    Dynamics and Control of the HELIOS Solar Sail Demonstrator

    15'

    confirmed

    Mr. Daniel Guerrant

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    3

    Research on EPDM insulation ablation by particle flow based on strength failure model for porous charring layer

    15'

    withdrawn

    Mr. Yue Chen

    Shanghai Space Propulsion Technology Research Institute

    China

    4

    Development Of A Lox/Lch4 Technology Demonstrator Based On Regenerative Cooling Throughout Validation Of Critical Design Aspects With Breadboards In The Framework Of The Hyprob Program

    15'

    confirmed

    Dr. Francesco Battista

    CIRA Italian Aerospace Research Center, Capua

    Italy

    4

    Development Of A Lox/Lch4 Technology Demonstrator Based On Regenerative Cooling Throughout Validation Of Critical Design Aspects With Breadboards In The Framework Of The Hyprob Program

    15'

    confirmed

    Dr. Francesco Battista

    CIRA Italian Aerospace Research Center, Capua

    Italy

    5

    Development of Hydrogen Peroxide Rockets at Alta S.p.A.: the Past, the Present and the Future

    15'

    confirmed

    Dr. Angelo Cervone

    Delft University of Technology (TU Delft)

    The Netherlands

    6

    Experimental Studies of the Effects of Baffles Geometry on High-frequency Combustion Instability of Liquid Rocket Engine

    15'

    no-show

    Mr. Longfei Li

    Xi'an Aerospace Propulsion Institute

    China

    7

    A study on the improvement of ignition and thrust repeatability of a micro solid propellant thruster array

    15'

    confirmed

    Mr. Daeban Seo

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    8

    Triangular Deployable Space Sail Fold Patterns and Sail Materials

    15'

    withdrawn

    Mr. Andrew Wolahan

    Cranfield University

    The Netherlands

    9

    Ceramic Matrix Composites for Improved Rocket Engine Combustion Chambers

    15'

    withdrawn

    Mr. David Lee

    California State University, Long Beach

    United States

    10

    Thrust dependency of microwave rocket on power density distributions of an incident millimeter wave beam

    15'

    confirmed

    Mr. Toshikazu Yamaguchi

    The University of TOKYO, Graduate school

    Japan

    11

    Slurry-propellant rocket propulsion. New design solutions for displacing gas-generator and reliable multistart

    15'

    confirmed

    Mr. Yulian Protsan

    The Laboratory of Advanced Jet Propulsion

    Ukraine

    12

    Reseach of the Oxidizer-Rich Preburner-Pipe System Dynamic Characteristics

    15'

    no-show

    Mr. Shang Liu

    China

    13

    Development of Fuel Leakage Detection Sensor In Space Propulsion System

    Poster

    confirmed

    Ms. FUNMILAYO OGUN

    National Space Research and Development Agency (NASRDA)

    Nigeria

    14

    Hybrid Diagnostics for Spacecraft Propulsion System

    Poster

    confirmed

    Mr. Xiaohui Peng

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    15

    OPTIMIZATION OF ASCENT TRAJECTORY AND MASS BUDGET PREDICTION FOR A LOW POWER EXPERIMENTAL ROCKET

    Poster

    confirmed

    Ms. Joy Amedu

    National Space Research and Development Agency (NASRDA)

    Nigeria

    Development of a Liquid Oxygen-Methane Technology Demonstrator Based on Regenerative Cooling in the Framework of the HYPROB Program

    with 14688

    Dr. Francesco Battista

    CIRA Italian Aerospace Research Centre

    Italy