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  • session 2

    Title

    Propulsion System (2)

    type

    oral

    Description

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

    Date

    2014-09-30

    Time

    09:45

    Room

    714B

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

    A6 SRM updated status on demonstrations activities

    15'

    confirmed

    Mr. Philippe Cloutet

    Herakles, Safran group

    France

    2

    Analysis of Pressure Spikes in Large Segmented Solid Rocket Booster Motor

    15'

    no-show

    Mr. KIRAN PINUMALLA

    Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA

    India

    3

    Evaluations of Data Reduction Methods for Hybrid Rockets

    15'

    confirmed

    Prof. Harunori Nagata

    Hokkaido University

    Japan

    4

    Small solid and hybrid thrusters development for trajectory correction on upper stage and spacecrafts

    15'

    no-show

    Mr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    5

    Alternative Thrust Modulation Techniques for Solid and Hybrid Rockets

    15'

    confirmed

    Dr. David Greatrix

    Ryerson University

    Canada

    6

    Hybrid Paraffin-based Technology Demonstrator in the Framework of the Italian Hyprob Program: Status of Design and Development Activities

    15'

    withdrawn

    Mr. Francesco Ferrigno

    Centro Italiano Ricerche Aerospaziali

    Italy

    7

    Hybrid CubeSat Propulsion System with Application to a Mars Aerocapture Demonstration Mission

    15'

    confirmed

    Ms. Elizabeth Jens

    Stanford University

    United States

    8

    development of high performance hybrid rocket engine with multi-section swirl injection method for space propulsion system

    15'

    confirmed

    Mr. Kengo Ohe

    Kyushu University

    Japan

    9

    An Advanced Hybrid Rocket Engine for an Alternative Upper Stage of the Brazilian VLM 1 LEO-Launcher

    15'

    confirmed

    Dr. Ognjan Bozic

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

    Germany

    10

    Benefits of a hybrid propulsion system utilizing in situ produced oxidizer for a Mars Ascent Vehicle

    15'

    withdrawn

    Dr. Ashley Karp

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    11

    Numerical Simulation and Experimental Testing on Segmented Grain Hybrid Rocket Motor

    15'

    no-show

    Mr. Pengfei Wang

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    12

    theoretical and experimental investigation of multiple catalyst ignition of hydrogen peroxide hybrid rocket motor

    15'

    withdrawn

    Mr. Sheng Zhao

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    investigation of ignition transient process inside a longitudinal solid propellant crack

    15'

    withdrawn

    Prof. Bing Sun

    Beijing University of Aeronautics and Astronautics (BUAA)

    China