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  • session 2

    Title

    Propulsion System (2)

    Description

    This session is dedicated to all aspects of Solid and Hybrid Propulsion.

    Date

    2015-10-13

    Time

    09:45

    Room

    Ballroom B (Crowne Plaza Hotel, -1 floor)

    IPC members
    • Co-Chair: Mr. Stéphane Henry, ArianeGroup, France;

    • Co-Chair: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;

    • Rapporteur: Mr. M. Badrinayarana Murthy, Indian Space Research Organization (ISRO), India;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    Advanced Biological Treatment for Solid Propulsion - LICORNE

    15'

    confirmed

    Mr. Guillaume Dupouy

    Herakles (Safran group)

    France

    2

    10:00

    A scaled-down static test method for solid rocket motors.

    15'

    confirmed

    Ms. Olga Motsyk

    Delft University of Technology (TU Delft)

    The Netherlands

    3

    10:15

    improvement on thrust profile flexibility by oxidizer-to-fuel ratio feedback control in hybrid rocket

    15'

    confirmed

    Mr. Tomoaki Usuki

    Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency

    Japan

    4

    10:30

    HEAT AND MASS TRANSFER ANALYSIS FOR PARAFFIN / NITROUS OXIDE BURNING RATE IN HYBRID PROPULSION

    15'

    confirmed

    Mrs. Shani Ben-Basat

    TECHNION - Israel Institute of Technology

    Israel

    5

    10:45

    Performance Calculations and Burning Tests on Altering-intensity Swirling Oxidizer Flow Type Hybrid Rocket Engines

    15'

    confirmed

    Mr. Kohei Ozawa

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan

    6

    11:00

    PRELIMINARY DESIGN OF HYBRID GAS GENERATOR IN STAGED HYBRID ROCKET ENGINE

    15'

    confirmed

    Prof. Changjin Lee

    Konkuk University

    Korea, Republic of

    7

    11:15

    Integrated approach for hybrid rocket technology development and analysis of possible applications

    15'

    confirmed

    Dr. Francesco Barato

    University of Padova - DII/CISAS

    Italy

    8

    11:30

    Combustion Instability in SARA Hybrid Rocket Motor

    15'

    confirmed

    Prof. Artur Bertoldi

    University of Brasilia

    Brazil

    9

    11:45

    Design of a hybrid paraffin-based technology demonstrator

    15'

    confirmed

    Dr. Marco Di Clemente

    CIRA Italian Aerospace Research Centre

    Italy

    10

    12:00

    Benefits of a Hybrid Propulsion System Using In Situ Produced Oxidizer for a Mars Ascent Vehicle

    15'

    withdrawn

    Dr. Ashley Karp

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    11

    12:15

    Combustion Instability Simulation and Analysis of a Solid Rocket Motor Testing Device based on LES Method

    15'

    confirmed

    Mr. Linqing Zhang

    The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp

    China

    12

    12:30

    estimation of flight specific impulse for solid propellant rocket motors

    15'

    withdrawn

    Mr. Chamarthi Sainadh

    ISRO

    India