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  • session 8-B4.5A

    Title

    Joint Session between IAA and IAF for Small Satellite Propulsion Systems

    Description

    This session will pay particular attention to propulsion systems and associated technologies as an enabler to efficient small satellite access to space and orbit change. Papers are invited discussing the particular challenges of design, manufacture, testing, operations and technological developments of small satellite propulsion systems, and the challenges of obtaining high performance within a small volume and mass. The scope includes chemical and electrical propulsion systems for major orbit changes, fine orbit control and maintenance, and end-of-life disposal. For papers with an emphasis on the small satellite and its system design, refer to other B4 sessions. For a focus on other propulsion systems and technologies, refer to other C4 sessions.

    IPC members
    • Co-Chair: Dr. Arnau Pons Lorente, Space Generation Advisory Council (SGAC), United States;

    • Co-Chair: Dr. Jeff Emdee, The Aerospace Corporation, United States;

    • Rapporteur: Dr. Elena Toson, T4i, Italy;

    • Rapporteur: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Design of CubeSat propulsion system using hydrogen peroxide monopropellant thruster

    10

    confirmed

    Mr. Seungho Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    2

    MIMPS-G: Modular Impulsive Green-Monopropellant Propulsion System for Micro/Nano Satellites High-thrust demanding Orbital Maneuvers.

    10

    confirmed

    Mr. Ahmed E. S. NOSSEIR

    Delft University of Technology (TU Delft)

    The Netherlands

    3

    Test campaign of a Cubesat equipped with an helicon plasma thruster

    10

    confirmed

    Dr. Fabrizio Stesina

    Politecnico di Torino

    Italy

    8

    development of a six-directional plasma propulsion module for small satellites

    10

    confirmed

    Mr. Andrei Shumeiko

    Bauman Moscow State Technical University

    Russian Federation

    11

    Flow regime characterization of a MEMS-based vaporizing liquid microthruster

    10

    confirmed

    Mr. Donato Fontanarosa

    Università del Salento

    Italy

    12

    Sulfur-fueled Surface Arc Thruster for Propelling Nanosatellites

    10

    confirmed

    Mr. Senior Shimhanda

    Kyushu Institute of Technology

    Japan

    13

    Initial Modelling of Cubesat Constellation Dispersal, Comparing Diverse Propulsion Technologies

    10

    confirmed

    Dr. Patrick Neumann

    Space Industry Association of Australia

    Australia