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  • session 6

    Title

    New Missions Enabled by New Propulsion Technology and Systems

    Description

    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.

    Date

    2017-09-28

    Time

    14:45

    Room

    Hall E3

    IPC members
    • Co-Chair: Mr. Giorgio Saccoccia, Italian Space Agency (ASI), Italy;

    • Co-Chair: Dr. Jerrol Littles, Aerojet Rocketdyne, United States;

    • Rapporteur: Mrs. Elena Toson, Space Generation Advisory Council (SGAC), Italy;

    • Rapporteur: Dr. Alexander Lovtsov, SSC Keldysh Research Centre, Russian Federation;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    Using linear electromagnetic acceleration of satellite payloads for targeted atmospheric injection and orbital trajectory adjustment

    15

    withdrawn

    Mr. Hugh Carrigg

    Australia

    2

    15:00

    Application for Spacecraft in Very Low Orbits Based on Air-Breathing Electric Propulsion System

    15

    no-show

    Mr. xiaoye wang

    Lanzhou Institute of Physics, China Academy of Space technology

    China

    3

    15:15

    Design and Development of a Sublimating Solid Propellant Tank for CubeSat and PocketQube Applications

    15

    confirmed

    Mr. Didier Maxence

    Delft University of Technology (TU Delft)

    The Netherlands

    4

    15:30

    Electrodynamic wing for LEO spacecraft propulsion

    15

    confirmed

    Prof. Jianguo Huang

    Beijing Institute of Spacecraft Environment Engineering

    China

    5

    15:45

    SYSTEM ANALYSIS AND TEST-BED FOR AN ATMOSPHERE-BREATHING ELECTRIC PROPULSION SYSTEM USING AN INDUCTIVE PLASMA THRUSTER

    15

    confirmed

    Mr. Francesco Romano

    Institute of Space Systems, University of Stuttgart

    Germany

    6

    16:00

    Feasibility of an Integrated Solar Thermal Power and Propulsion System for Small Satellites

    15

    confirmed

    Ms. Fiona Leverone

    Delft University of Technology (TU Delft), The Netherlands

    The Netherlands

    7

    16:15

    Electric propulsion for high-power deep space transportation system: investigation on mutual influences and preliminary sizing

    15

    confirmed

    Ms. Martina Mammarella

    Politecnico di Torino

    Italy

    8

    16:30

    Stationkeeping with an electrospray propulsion system for low lunar polar mission on a 6U CubeSat

    15

    confirmed

    Mr. Michele Benetti

    Politecnico di Milano

    Italy

    9

    16:45

    Unique Advantages of Hybrid Rocket Technology for Mars Missions

    15

    no-show

    Prof.Dr. arif karabeyoglu

    Koc University

    United States

    10

    17:00

    Finding NewSpace: Mission Scenarios Utilizing LOTUS: Lander/Orbiter Trans-Upper Stage

    15

    confirmed

    Mr. Chrishma Singh-Derewa

    National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory

    United States

    11

    17:15

    Overview and Analysis of Msail and Esail Propulsion for Interplanetary Misions

    15

    confirmed

    Prof. Harijono Djojodihardjo

    Indonesia

    12

    17:30

    Increasing the Accuracy of Electric Sail Mission Performance Estimates

    15

    confirmed

    Mr. Thomas Gemmer

    North Carolina State University

    United States