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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

    2018-10-04

    Time

    13:15

    Room

    IP Hall

    IPC members
    • Co-Chair: Mr. Christophe Bonnal, European Conference for Aero-Space Sciences (EUCASS), France;

    • Co-Chair: Mr. Daniel L. Dumbacher, American Institute of Aeronautics and Astronautics (AIAA), United States;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A new three-stage-to-orbit vehicle concept utilizing rocket-based combined cycle propulsion

    10

    confirmed

    Mr. Cong Zhou

    School of Astronautics,Northwestern Polytechnical University

    China

    2

    Economic analysis of reusable launch vehicle system

    10

    withdrawn

    Dr. Sheng Zhao

    China Academy of Launch Vehicle Technology (CALT)

    China

    3

    Maturity Assessment Process for USAF New Entrant Launch Systems

    10

    confirmed

    Mr. Jeffrey Michlitsch

    The Aerospace Corporation

    United States

    4

    Theoretical and experimental studies of technology development of launch vehicles (LV) with improved environmental characteristics on the example of promising LV launched from the Baikonur cosmodrome

    10

    Prof. Valery Trushlyakov

    Omsk State Technical University

    Russian Federation

    5

    Trajectory Optimization for Powered Descent and Landing of Reusable Rockets with Restartable Engines

    10

    confirmed

    Dr. Lin Ma

    Zhejiang University

    China

    6

    Research on Aero-space Vehicle using Air-breathing Combined Engine and Conceptual Vehicle Design

    10

    confirmed

    Ms. Ning Zhou

    China Aerospace Science & Industry Corporation (CASIC)

    China

    7

    AN IMPROVED REENTRY TRAJECTORY OPTIMIZATION METHOD FOR MULTIPLE NO-FLY ZONES AND WAYPOINTS

    10

    withdrawn

    Mr. Mu yin Tian

    Beihang University (BUAA)

    China

    8

    Atmospheric Powered Descent Guidance for Rockets Precision Landing on Earth

    10

    confirmed

    Mr. Qingzhong Gan

    Shanghai Aerospace Control Technology Institute (SACTI), Shanghai Academy of Spaceflight Technology (SAST)

    China

    9

    Development of a Suborbital Inexpensive Rocket for Affordable Space Access

    10

    confirmed

    Mr. Hamed Gamal

    SpaceForest

    Poland

    10

    A Novel Software Application for the Design and Optimization of Student Launch Vehicles

    10

    Mr. Mark Snidal

    Concordia University

    Canada

    11

    cfd based method for modeling convection within thermal system analysis tools for launchers

    10

    confirmed

    Dr. Christian Wendt

    ArianeGroup

    Germany

    12

    Launch Environment Measurement CubeSat and Lessons Learned

    10

    confirmed

    Ms. Arielle Cohen

    California Polytechnic State University

    United States

    13

    MULTIDISCIPLINARY SHAPE OPTIMIZATION OF FUTURE REUSABLE SPACE VEHICLE

    10

    withdrawn

    Mr. Sagar Satpathy

    Politecnico di Milano

    Italy

    14

    Optimization of 2 stage boosted dart suborbital vehicle

    10

    Mr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    15

    Performance Optimization of the Methanol/LOX Sounding Rocket Systems

    10

    confirmed

    Mr. Naser Ashknani

    Kuwait University

    Kuwait

    16

    Low-Cost Prototype Development of a Lunar Massdriver

    10

    confirmed

    Mr. Manfred Ehresmann

    Institute of Space Systems, University of Stuttgart

    Germany

    17

    orbital transfer performance analysis for momentum exchange tether based spacecraft system

    10

    confirmed

    Dr. Feng Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    18

    Space "filling station

    10

    confirmed

    Dr. Sergiy Matviyenko

    JSC "RPC "KURS"

    Ukraine