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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: Mr. Arnau Pons Lorente, Purdue University, United States;

    • Co-Chair: Dr. Jeffery 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

    15

    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.

    15

    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

    15

    confirmed

    Dr. Fabrizio Stesina

    Politecnico di Torino

    Italy

    4

    Multiphase flow modeling in micro-thruster using lattice Boltzmann method

    15

    withdrawn

    Mr. Julius Weinmiller

    Delft University of Technology (TU Delft)

    The Netherlands

    5

    Development of a Microscale Heating Mechanism for a Small Satellite Resistojet Thruster

    15

    Mr. Bradley Hoover

    United States

    6

    Application to satellite of a direct-injection gas-hybrid rocket system using glycidyl azide polymer and nitrous oxide

    15

    Mr. Shintaro Hatano

    Chiba Institute of Technology

    Japan

    7

    Development of Water Propulsion Systems for small-scale Satellites

    15

    withdrawn

    Mr. Razvan Nicoara

    COMOTI

    Romania

    8

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

    15

    confirmed

    Mr. Andrei Shumeiko

    Bauman Moscow State Technical University

    Russian Federation

    9

    Design and Analysis of a MEMS based Microvalve for Micro-propulsion Systems

    15

    Ms. Shrutika Agarwal

    TU Delft

    The Netherlands

    10

    Autophage Small Satellite Engine Lab Version Test Results

    15

    confirmed

    Mr. Mykhailo Yemets

    Oles Honchar Dnipropetrovsk National University

    Ukraine

    11

    Flow regime characterization of a MEMS-based vaporizing liquid microthruster

    15

    confirmed

    Mr. Donato Fontanarosa

    Università del Salento

    Italy

    12

    Sulfur-fueled Surface Arc Thruster for Propelling Nanosatellites

    15

    confirmed

    Mr. Senior Shimhanda

    Kyushu Institute of Technology

    Japan

    13

    Initial Modelling of Cubesat Constellation Dispersal, Comparing Diverse Propulsion Technologies

    confirmed

    Dr. Patrick Neumann

    Space Industry Association of Australia

    Australia

    14

    Thrust augmentation and vectoring control in a planar micronozzle of micro-resistojets by means of secondary injection

    confirmed

    Mr. Donato Fontanarosa

    Università del Salento

    Italy

    15

    FLUIDIC THRUST VECTORING IN SMALL SATELLITES BY EMPLOYING COMBINED SHOCK VECTORING AND SONIC PLANE SKEWING TECHNIQUE TO DUAL THROAT NOZZLE.

    confirmed

    Ms. Shreesha Madhu

    R.V.College of Engineering

    India