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  • session 2

    Title

    Propulsion System (2)

    Description

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

    Date

    2013-09-24

    Time

    09:45

    Room

    208A

    IPC members
    • Chairman: Mr. Stéphane Henry, ArianeGroup, France;

    • Chairman: Dr. I-Shih Chang, The Aerospace Corporation, United States;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Solid rocket motors choices for Ariane 6 launcher

    15'

    confirmed

    Mr. Didier Boury

    Herakles (Safran group)

    France

    2

    Demonstration Technology Activities for Ariane 6 PPH Solid Rocket Motors Stages

    15'

    confirmed

    Mr. Philippe Cloutet

    Herakles, Safran group

    France

    3

    Characterization of the Ballistic Properties of the Novel ALAN-7 Solid Rocket Propellant

    15'

    confirmed

    Mr. Hein Olthof

    Delft University of Technology (TU Delft)

    The Netherlands

    4

    experimental investigation of the pressure coupled responses of composite propellant with different ammonium perchlorate particles size

    15'

    confirmed

    Mr. Bingning Jin

    Northwestern Polytechnical University

    China

    5

    Development of the Quasi-3D Model for the Grain Burnback Analysis of SRM's

    15'

    confirmed

    Mr. Arnau Pons Lorente

    Escola Tècnica Superior d'Enginyeries Industrial i Aeronàutica de Terrassa (ETSEIAT), Universitat Politècnica de Catalunya

    China

    6

    Multi-objective Optimization of Hybrid Rocket Motor and Decision-making Using a Hyper-Radial Visualization Method

    15'

    confirmed

    Mr. Xingliang Sun

    Beijing University of Areonautics and Astronautics

    China

    7

    experimental investigation on a lab-scale hybrid rocket burning N2O/paraffin-based fuel and N2O/metal-loaded HTPB

    15'

    confirmed

    Ms. Francesca Scaramuzzino

    Second University of Naples, SUN

    Italy

    8

    Visualization of Hybrid Combustion between Paraffin and Gaseous Oxygen

    15'

    withdrawn

    Ms. Elizabeth Jens

    Stanford University

    United States

    9

    Observation of the surface regression behavior of hybrid rocket fuel using a slab motor

    15'

    confirmed

    Dr. Yutaka Wada

    Akita University

    Japan

    10

    Regression Rate Models versus experimental Results for Hybrid Rocket Engines based on H2O2 and HTPB/Al

    15'

    confirmed

    Mr. Dennis Porrmann

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

    Germany

    11

    Numerical Simulation of Unsteady Non-Equilibrium Flows of Hybrid Rocket Ignition using Size-Optimized Reaction Mechanism

    15'

    confirmed

    Mr. Shota Yamanaka

    University of Tokyo

    Japan

    12

    Aspects regarding hybrid combustion instability control

    15'

    confirmed

    Prof. Sterian Danaila

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania