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  • session 5

    Title

    Propulsion Technology (2)

    Description

    This session includes all science and technologies supporting all aspects of space propulsion. An objective is to attract papers from students and young professionals with a more technical rather than programmatic or organisational focus.

    Date

    2016-09-29

    Time

    09:45

    Room

    Zapopan

    IPC members
    • Co-Chair: Mr. Walter Zinner, ArianeGroup, Germany;

    • Co-Chair: Mr. Jacques Gigou, European Space Agency (ESA), France;

    • Rapporteur: Mr. Zvika Zuckerman, Rafael Advanced Defense Systems Ltd., Israel;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    investigation on exhaust plume radiation of lox/kerosene rocket engine

    15'

    confirmed

    Dr. Yuanqi Li

    Xian Aerospace Propulsion Institute

    China

    2

    Structural dynamic analysis of 18,000-kg thrust LOX/Kerosene engine

    15'

    confirmed

    Mr. song yan

    Xi'an Aerospace Propulsion Institute

    China

    3

    simulation of the vortex-cooled thrust chamber based on gaseous oxygen and kerosene

    15'

    confirmed

    Mr. Yong Wang

    Xi'an Aerospace Propulsion Institute

    China

    4

    Evaluation of the Performance Potential of Aerodynamically Thrust Vectored Aerospike Nozzles

    15'

    confirmed

    Mr. Christian Bach

    Dresden University of Technology (DUT) / Technische Universität Dresden

    Germany

    5

    Design boundaries of a liquid-fuelled propulsion system for a 500 N sounding rocket

    15'

    confirmed

    Mr. Christian Bach

    Dresden University of Technology (DUT) / Technische Universität Dresden

    Germany

    6

    Parametric optimization of a bistable electromechanical valve actuator for tank pressurization

    15'

    confirmed

    Mr. Victor Casado

    Airbus Safran Launchers

    Germany

    7

    Development of Thermal Protection Boot For S200 Flex Seal of Large Solid Rocket Booster Flex Nozzle

    15'

    confirmed

    Mr. S KARTHEEKEYAN

    Vikram Sarabhai Space Centre (VSSC)

    India

    8

    Testing and Qualification of Booster Flex Seals For S200 Solid Rocket Booster

    15'

    confirmed

    Mr. S KARTHEEKEYAN

    Vikram Sarabhai Space Centre (VSSC)

    India

    9

    Paraffin-based fuels for hybrid propulsion: characterization of waxes and its blends.

    15'

    confirmed

    Ms. Anastasia Petrova

    Politecnico di Milano

    Italy

    10

    Research on Ablation Characteristic of EPDM Insulator in Use of Different Propellant

    15'

    confirmed

    Dr. Yiwen Guan

    Northwestern Polytechnical University,NPU

    China

    11

    Development of a Nitrous Oxide-Based Monopropellant Propulsion System for Small Satellites

    15'

    withdrawn

    Mr. Vincent Tarantini

    Space Flight Laboratory, University of Toronto

    Canada

    Processing Of Flex Seal For Large Solid Rocket Booster Flex Nozzle

    confirmed

    Mr. S KARTHEEKEYAN

    Vikram Sarabhai Space Centre (VSSC)

    India