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    Title

    Virtual 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.

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

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

    • Rapporteur: Mr. Markus Jaeger, Airbus Defence & Space, Space Systems, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Development Update on Modul Interplanetary Transport System (M-ITS)

    confirmed

    Mr. Rok Kete

    Slovenia

    2

    Guidance system design and verification for the small commercial rocket

    Dr. Wei Wang

    China Aerospace Science & Industry Corporation (CASIC)

    China

    3

    A new conceptual scheme for Air Launch Reusable Launch Vehicle (ALRLV)

    Dr. Hassan Naseh

    Aerospace Research Institute, Ministry of Science, Research and Technology

    Iran

    4

    Concept Design of an in-Orbit Propulsion System based on Magnetofluids

    confirmed

    Ms. Franziska Hild

    University of Stuttgart

    Germany

    5

    Design and verification of a rocket's mirroring system based on digital twin technology

    confirmed

    Mrs. Mengyun Yue

    Beijing Institute of Astronautical Systems Enginnering

    China

    6

    The Chinese first proposed inverted reuse scheme for a launcher’s first-stage using parachutes based on landing topography and tail rudder control system

    Mr. Ruikang Yang

    LandSpace Technology

    China

    7

    LAPLaS (Laser Ablation Propulsion Launch System) is an adequate solution for launching small payloads to LEO in SSTO, on-demand, low-cost and safe manner.

    Mr. IOURI PIGULEVSKI

    Switzerland

    8

    GENERALIZATION OF PERFORATED FORCED CONVECTION HEAT TRANSFER AND IMPLICATIONS ON AEROSPACE PROPULSION SYSTEMS

    confirmed

    Mr. Vinayak Malhotra

    SRM University Chennai

    India

    9

    Moon-Tram, or escape velocity without fossil rocket propellant ?

    Mr. Nandor Motruk

    Hungary

    10

    Trajectory co-simulation of launch vehicle powered by beamed energy propulsion and its relay satellites designed for micro-payload at LEO

    withdrawn

    Mr. Pengcheng Wang

    Beihang University (BUAA)

    China

    11

    Nanosats and suborbital feasible missions from a brazilian launch center

    confirmed

    Dr. Filipe Taveiros

    Barreira do Inferno Launch Center (CLBI)

    Brazil

    12

    Interplanetary Non-propulsive Transport System

    confirmed

    Mr. Navjeet Singroha

    University of Petroleum and Energy Studies

    India

    13

    Proposal of launcher recovery systems for small satellite missions

    Mr. Mauro Rojas

    Luleå University of Technology

    Czech Republic

    14

    Design and Fabrication of Reaction Control System for Model Rockets

    confirmed

    Mr. Shantanu Trivedi

    SRM University, kattankulathur, chennai, INDIA

    India

    15

    PROPULSION SYSTEM OF A NANOLAUNCHER BASED ON AEROSPIKE NOZZLE TO SEND CUBESATS FROM MEXICO

    confirmed

    Mr. Irving Enrique Gomez Fernandez

    Mexico

    16

    Comparison Study of Launch Vehicle Control Surfaces at Supersonic Speeds under Different Configurations using Computational Analysis

    confirmed

    Mr. Palaniappan Subramanian

    University of Petroleum and Energy Studies

    India

    17

    Development of a Flight Computer for High Power Amateur Rockets

    withdrawn

    Mr. Kevin Dick

    University of Manitoba

    Canada

    18

    Introducing Launch Operations of Korea New Launch Vehicle Based on Test Launch Vehicle Flight Test

    withdrawn

    Dr. Sunil Kang

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of