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  • session 2

    Title

    Propulsion System (2)

    Description

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

    Date

    2016-09-27

    Time

    09:45

    Room

    Zapopan

    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;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE:Green Solid propellants for civilian launchers

    30'

    confirmed

    Mr. Max Calabro

    The Inner Arch

    France

    2

    Development and qualification of S200 solid rocket booster for GSLV Mk-III

    15'

    confirmed

    Mr. Arun Krishnan

    Indian Space Research Organization (ISRO)

    India

    3

    design and development of flex nozzle for large solid booster

    15'

    confirmed

    Mr. V MAHESH

    Indian Space Research Organization (ISRO)

    India

    4

    Thrust Oscillations in Static Tests of Large Segmented Solid Booster of ISRO

    15'

    no-show

    Mr. KIRAN PINUMALLA

    Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA

    India

    5

    Enhanced Epsilon Launch Vehicle and Future Plan

    15'

    confirmed

    Mr. Hirotaka Uehara

    IHI Aerospace Co, Ltd.

    Japan

    6

    development of solid propulsion system for enhanced epsilon launch vehicle and M-35 static firing test

    15'

    confirmed

    Dr. Koki Kitagawa

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan

    7

    Performance Evaluation of Composite Propellant Slurry Mixing by Peristaltic Continuous Mixer

    15'

    confirmed

    Mr. Akihiro Iwasaki

    The Graduate Universty for Advanced Studies (SOKENDAI)

    Japan

    8

    modeling distributed combustion in srm

    15'

    no-show

    Prof. Domenico Simone

    University of Brasilia

    Brazil

    9

    Errosive burning modelling on solid rocket motors. Application to development of SRM 120.

    15'

    confirmed

    Mr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    10

    Secondary Combustion in Staged Hybrid Rocket Engine

    15'

    confirmed

    Mr. Dongeun Lee

    Konkuk University

    Korea, Republic of

    11

    Development of Module-Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Flight Experiments

    15'

    confirmed

    Prof. Shigeru Aso

    Kyushu University

    Japan

    12

    Verification of the Throttling Characteristics of Axial-injection End-burning Type Hybrid Rockets

    15'

    confirmed

    Mr. Yuji Saito

    Hokkaido University

    Japan

    13

    Flame Emission Spectroscopy in a Paraffin-Based Hybrid Rocket

    15'

    confirmed

    Mr. Keith Stober

    Stanford University

    United States

    14

    A test bench for the characterization of solid rocket engines: Design, construction and validation

    15'

    withdrawn

    Dr. Javier M. Antelis

    TECNOLOGICO DE MONTERREY

    Mexico