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  • session IP

    Title

    Interactive Presentations - IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

    Description

    This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Space Transportation Solutions and Innovations addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the D Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.

    Date

    2019-10-24

    Time

    13:15

    Room

    IP Area

    IPC members
    • Co-Chair: Mr. Christophe Bonnal, Centre National d'Etudes Spatiales (CNES), France;

    • Co-Chair: Dr. Jens Lassmann, ArianeGroup, Germany;

    • Rapporteur: Mrs. Philippa Davies, Reaction Engines Ltd., United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    13:15

    Development of KSLV-II and flight test of its one staged test vehicle employing newly developed main engine(KRE-75)

    Dr. seung-bo jin

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    2

    13:15

    the design and development of a medium-scale liquid commercial launch vehicle named zq-2 based on liquid oxygen and liquid methane propulsion system

    confirmed

    Mr. YAWEI XU

    LandSpace Technology Ltd

    China

    3

    13:15

    Multidisciplinary design analysis of a semi-reusable two-stage-to-orbit small payload launch system

    confirmed

    Dr. Christie Maddock

    University of Strathclyde

    United Kingdom

    4

    13:15

    Lessons and Learns of Launching Test Launch Vehicle of KSLV-II concerning Launch Complex Development

    Dr. Sunil Kang

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    5

    13:15

    Orbit Transfer Analysis with a 3D Vis-Viva Equation

    Mr. Manfred Ehresmann

    Institute of Space Systems, Universität Stuttgart

    Germany

    6

    13:15

    Lightning Protection System: current strategy and evolutions

    Mr. Gérard ORDONNEAU

    ONERA - The French Aerospace Lab

    France

    7

    13:15

    suboptimal rocket landing guidance using model predictive static programming

    Mr. Cong Zhou

    School of Astronautics,Northwestern Polytechnical University

    China

    8

    13:15

    Comparative analysis of upper stage and built-in propulsion system for GEO satellite launches

    confirmed

    Mr. Roman Mykhalchyshyn

    Yuzhnoye State Design Office

    Ukraine

    9

    13:15

    Technical Improvement of Launch Vehicle Control System for Chang'e 4 Mission

    Mr. Xiaopeng Shang

    Beijing Aerospace Automatic Control Institute

    China

    10

    13:15

    Autophage nanolauncher - a solid SSTO launch vehicle

    Dr. Patrick Harkness

    School of Engineering, University of Glasgow

    United Kingdom

    11

    13:15

    Nanosats and Suborbital Feasible Missions from a Brazilian Launch Center

    Dr. Filipe Taveiros

    Barreira do Inferno Launch Center (CLBI)

    Brazil

    12

    13:15

    Guidance system design and verification for the small commercial rocket

    Dr. Wei Wang

    China Aerospace Science & Industry Corporation (CASIC)

    China

    12

    13:15

    Overview of Avionics Architecture on Stand-alone Test Launch Vehicle (TLV), Second Stage of Korea Space Launch Vehicle-II (KSLV-II)

    Dr. Seung-Hyun Hwang

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of