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    IAC-16 — 67th International Astronautical Congress

    C4. SPACE PROPULSION SYMPOSIUM

    The Space Propulsion Symposium addresses sub-orbital, Earth to orbit and in-space propulsion. The general areas considered include both chemical and non-chemical rocket propulsion, air-breathing propulsion, and combined air-breathing and rocket systems. Typical specific propulsion categories of interest are liquid, sold and hybrid rocket systems, ramjet, scramjet, and various combinations of air-breathing and rocket propulsion and nuclear, electric, solar and other advanced rocket systems. The Symposium is concerned with component technologies, the operation and application to missions of overall propulsion systems and unique propulsion test facilities.

    Coordinator

    Toru Shimada
    Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency — Japan

    Helen Webber
    Reaction Engines Ltd. — United Kingdom

    Giorgio Saccoccia
    Vast — France

    Christophe Bonhomme
    Centre National d'Etudes Spatiales (CNES) — France

    Riheng Zheng
    Beihang University — China

    C4.1. Propulsion System (1)

    This session is dedicated to all aspects of Liquid Rocket Engines.

    Co-Chair

    Christophe Bonhomme
    Centre National d'Etudes Spatiales (CNES) — France

    Patrick Danous
    ArianeGroup — France

    C4.2. Propulsion System (2)

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

    Co-Chair

    Stéphane Henry
    — France

    Toru Shimada
    Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency — Japan

    C4.3. Propulsion Technology (1)

    This session included all science and technologies supporting all aspects of space propulsion. The emphasis in this session is plased in particular components for propulsion.

    Co-Chair

    Didier Boury
    ArianeGroup SAS — France

    Angelo Cervone
    Delft University of Technology (TU Delft) — Netherlands (Kingdom of the)

    Rapporteur

    John Harlow
    Aerojet Rocketdyne — United Kingdom

    C4.4. Electric Propulsion

    This session is dedicated to all aspects of electric propulsion technologies, systems and applications.

    Co-Chair

    Garri A. Popov
    Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI — Russian Federation

    Vanessa Vial
    SAFRAN — France

    Rapporteur

    Norbert Puettmann
    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR) — Germany

    C4.5. Propulsion Technology (2)

    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.

    Co-Chair

    Walter Zinner
    ArianeGroup — Germany

    Jacques Gigou
    European Space Agency (ESA) — France

    Rapporteur

    Zvika Zuckerman
    Rafael Advanced Defense Systems Ltd. — Israel

    C4.6. New Missions Enabled by New Propulsion Technology and Systems

    The session will explore concepts for new missions that can be enabled by specific advancements in propulsion and/or integration of various propulsion technologies and systems.

    Co-Chair

    Giorgio Saccoccia
    Vast — France

    Jerrol Littles
    Aerojet Rocketdyne — United States

    Rapporteur

    Mariano Andrenucci
    Independent consultant — Italy

    C4.7-C3.5. Joint Session on Nuclear Propulsion and Power

    This session, organised jointly between the Space Power and the Space Propulsion Symposium, includes papers addressing all aspects related to nuclear power and propulsion for space applications.

    Co-Chair

    Jerome Breteau
    European Space Agency (ESA) — France

    Leopold Summerer
    European Space Agency (ESA) — Netherlands (Kingdom of the)

    Rapporteur

    George Schmidt
    NASA Glenn Research Center — United States

    Vito Salvatore
    CIRA Italian Aerospace Research Center, Capua — Italy

    C4.8. Advanced Propulsion Systems

    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.

    Co-Chair

    Constanze Syring
    Deutsche Gesellschaft für Luft-und Raumfahrt, Lilienthal-Oberth e.V. (DGLR) — Germany

    Salvatore Borrelli
    CIRA Italian Aerospace Research Centre — Italy

    Rapporteur

    Youngbin Yoon
    Seoul National University — Republic of Korea

    C4.9. Hypersonic and Combined Cycle Propulsion

    This session covers papers on Hypersonic and Combined Cycle Propulsion for space applications.

    Co-Chair

    Helen Webber
    Reaction Engines Ltd. — United Kingdom

    Riheng Zheng
    Beihang University — China

    Rapporteur

    Salvatore Borrelli
    CIRA Italian Aerospace Research Centre — Italy

    C4.IP. Interactive Presentations

    Authors with an abstract accepted for an interactive presentation will be asked to prepare slides and display them for the duration of the congress on plasma screens. Authors will be assigned to interactive sessions in which they must be near the plasma screens to engage in interactive discussions with other congress attendees.

    Coordinator

    Giorgio Saccoccia
    Vast — France

    Toru Shimada
    Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency — Japan

    Helen Webber
    Reaction Engines Ltd. — United Kingdom

    Christophe Bonhomme
    Centre National d'Etudes Spatiales (CNES) — France

    Riheng Zheng
    Beihang University — China