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  • session 8

    Title

    Advanced and Combined Propulsion Systems

    Description

    The session is for the presentation of advanced propulsion concepts being studied or considered. The advanced concepts should seek to deliver breakthroughs in overcoming the limitations of propulsion systems in current use or development. For advanced concepts technologies should normally be in the range TRL 0 to TRL 2. Advanced concepts with higher TRL technologies may also be presented where a combination of propulsion technologies can lead to performance breakthroughs which can not be achieved with a single technology. A combination can include for example both chemical and electric or solid and liquid chemical.

    Date

    2014-10-03

    Time

    13:30

    Room

    714B

    IPC members
    • Co-Chair: Prof. Youngbin Yoon, Seoul National University, Korea, Republic of;

    • Co-Chair: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

    • Rapporteur: Mrs. Constanze Syring, Deutsche Gesellschaft für Luft-und Raumfahrt, Lilienthal-Oberth e.V. (DGLR), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Introduction and Performance Analysis of the Solar Wind Ion Focusing Thruster (SWIFT)

    20'

    confirmed

    Mr. Thomas Gemmer

    North Carolina State University

    United States

    2

    orbital maneuver of satellite using solar sail

    20'

    no-show

    Mr. Logesh Sadasivam

    SRM University, kattankulathur,chennai,INDIA

    India

    3

    optimal design of conduction-cooled superconducting magnet for magneto plasma sail

    20'

    confirmed

    Mr. Yoh Nagasaki

    Research Institute for Sustainable Humanosphere, Kyoto University

    Japan

    4

    SOLAR ELECTRO REACTION ENGINE

    20'

    no-show

    Ms. Safoora Tanbakouei

    Space Generation Advisory Council (SGAC)

    Iran

    5

    Second Generation EmDrive Propulsion applied to SSTO Launcher and Interstellar Probe.

    20'

    confirmed

    Mr. Roger Shawyer

    Satellite Propulsion Research Ltd

    United Kingdom

    6

    Creation of LPRE with the use of detonation combustion in the chamber

    15'

    withdrawn

    Mr. Vladimir Sudakov

    JSC NPO Energomash

    Russian Federation

    7

    Numerical Simulation of Combustion Characteristics of Boron Particle in Forced Convective Environment

    20'

    no-show

    Mr. Chuanbo Fang

    National University of Defense Technology

    China

    8

    High Resolution Numerical Simulation on Dynamics of Intake Shock Motion

    20'

    confirmed

    Ms. Qin Yan-ping

    Xi'an Aerospace Propulsion Institute

    China