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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

    2013-09-27

    Time

    13:30

    Room

    208A

    IPC members
    • Chairman: Mr. Jacques Gigou, European Space Agency (ESA), France;

    • Chairman: Mr. Richard Blott, British Interplanetary Society, United Kingdom;

    • Rapporteur: Mr. William W. Smith, Aerojet Rocketdyne, United States;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

    radio wave and ion cyclotron thruster

    Mr. Harshit Bisen

    SRM University Chennai

    India

    2

    confirmed

    15'

    A NOVEL COMBINED PROPULSION CONCEPT FOR DEEP SPACE MISSIONS

    Ms. Ragini Ramachandran

    Embry Riddle Aeronautical University

    United States

    3

    confirmed

    15'

    FAST Z-PINCH THRUSTER FOR SPACE TUGS

    Mr. Patrick Giddens

    UAHuntsville

    United States

    4

    confirmed

    15'

    Experimental tests of the Mach Effect Thruster.

    Prof. Heidi Fearn

    California State University

    United States

    5

    15'

    ADVANCED SOLAR THERMAL PROPULSION WITH SPECTRAL-SELECTIVE MULTI-STAGED CONCENTRATOR-ABSORBER SYSTEM

    Prof. Sergey Finogenov

    Moscow Aviation Institute

    Russian Federation

    6

    confirmed

    15'

    Investigation on Status and Prospective Application of Gelled Propellants

    Dr. Shuang Liu

    The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp

    China

    7

    withdrawn

    15'

    A Study of Laser propulsion: An Overdriven detonation mode for a laser-absorption wave

    Mr. Joseph Ofosu

    University of Tokyo

    Japan

    8

    15'

    Numerical study on working processes of a novel laser ablation thruster with electromagnetic acceleration

    Mr. Daixian Zhang

    College of Aerospace Science and Engineering, National University of Defense Technology

    China

    9

    withdrawn

    15'

    LightForce: Refined Laser Propulsion Force Model

    Mr. Fan Yang Yang

    National Aeronautics and Space Administration (NASA), Ames Research Center / USRA

    United States

    10

    15'

    Experimental Research on Continuous Detonation Engine

    Mr. Tianyi Shi

    Peking University Health Science Center

    China

    11

    15'

    Effects of Different Types of Diverging Nozzle on Propulsion Performance of Continuous Detonation Engine (CDE)

    Dr. Ugur Guven

    United States

    12

    confirmed

    15'

    optimum control of ramjets at high flight Mach number and wide-range working conditions

    Ms. Baoe Yang

    Xi'an Aerospace Propulsion Institute

    China