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  • session 8

    Title

    Advanced and Combined Propulsion Systems

    type

    oral

    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

    2012-10-05

    Time

    14:00

    Room

    TS14 (Sala Capri, Palacongressi)

    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

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Deep space exploration using airbreathing antimatter(positronic) propulsion for single-stage-to orbit missions

    15'

    confirmed

    Mr. Anirudh Thimmaiah

    India

    2

    Competing evolution of engines, power installations and mobile starting complexes under scenarios of atmospheric and space prospects

    15'

    confirmed

    Prof. igor Kurkin

    Moscow Aviation Institute

    Russian Federation

    3

    Application of the Continuous Rotating Detonation to Jet and Rocket Propulsion

    15'

    confirmed

    Prof. Piotr Wolanski

    Polish Academy of Sciences

    Poland

    4

    Project Icarus: Analysis of Magnetic Nozzle Design for a Pulsed-Fusion Propulsion System

    15'

    confirmed

    Mr. Richard Hatcher

    Propulsion Research Center, University of Alabama in Huntsville

    United States

    5

    Numerical study of tubular heat exchanger in the air-breathing engine with manifold

    15'

    withdrawn

    Mr. KIM SANGJO

    Pusan National University

    Korea, Republic of

    6

    Design and Performance Study of A New Laser-electromagnetic Coupling Plasma Thruster

    15'

    confirmed

    Mr. Daixian Zhang

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

    China

    7

    Developments of microwave rocket as a future low-cost mass transportation system

    15'

    confirmed

    Mr. Toshikazu Yamaguchi

    The University of TOKYO, Graduate school

    Japan

    8

    Mixing enhancement in Hybrid rocket motor using vortex generators

    15'

    confirmed

    Prof. Fulvio Stella

    Universita' di Roma 'La Sapienza'

    Italy

    9

    Pulsed Micro-thrust Measurement Using Torsional Pendulum Techniques

    15'

    withdrawn

    Mr. Daixian Zhang

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

    China

    10

    Study of laser propulsion: one-dimensional modeling of Laser-Supported Detonation

    15'

    confirmed

    Mr. Toshikazu Yamaguchi

    Japan

    11

    Two- and three-dimensional particle-in-cell simulation of magneto plasma sail

    15'

    confirmed

    Mr. yasumasa ashida

    Research Institute for Sustainable Humanosphere, Kyoto University

    Japan

    12

    Numerical Investigation on Laser Ablation Characteristics of PTFE in Advanced Propulsion Systems

    15'

    withdrawn

    Mr. Daixian Zhang

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

    China