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  • session 5A-C4.8

    Title

    Joint Session between IAA and IAF for Small Satellite Propulsion Systems

    type

    oral

    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 electric propulsion systems for major orbit changes, fine orbit control and maintenance, and end-of-life disposal. This session will be accepting submissions for oral presentations only. 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.

    Date

    2024-10-17

    Time

    15:00

    Room

    Blue Hall 1

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

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

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

    • Rapporteur: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Development of a Bipropellant HTP - Propane Propulsion Subsystem for EARS (European Advanced Reusable Satellite) Program.

    12

    confirmed

    Mr. Lorenzo Gerolin

    T4i

    Italy

    2

    15:12

    In-Orbit Demonstration of a Steam-Powered Propulsion System

    12

    confirmed

    Dr. Marco Pavan

    United Kingdom

    3

    15:24

    Electromagnetic and Extended Vibrational Qualification Campaign for an Improved Centre-Triggered Pulsed Cathodic Arc Thruster

    12

    confirmed

    Dr. Patrick Neumann

    Australia

    4

    15:36

    Powderization of combustion products in magnesium-wire and water micropropulsion system: proof of concept

    12

    confirmed

    Mr. Minwoo Han

    The University of TOKYO, Graduate school

    Japan

    5

    15:48

    research and in-orbit verification on the han propulsion system of dalian-1 lianli satellite

    12

    confirmed

    Prof. Xiaozhou Yu

    Dalian University of Technology (DUT)

    China

    6

    16:00

    The Fully Wireless Six-degree-of-freedom Thrust Measurement for CubeSat Class Propulsion Systems

    12

    confirmed

    Mr. Ten Arai

    The University of TOKYO, Graduate school

    Japan

    7

    16:12

    In-flight Performance of Water Resisitojet Thruster AQUARIUS; from Long-term Trend to Space Environmental Effect

    12

    confirmed

    Mr. Aoma Fujimori

    Department of Engineering, The University of Tokyo

    Japan

    8

    16:24

    Lessons Learned from the Initial Operations Phase in the NanoFF CubeSat Formation Flight Mission

    12

    confirmed

    Mr. Debdeep Roychowdhury

    Technische Universität Berlin

    Germany

    9

    16:36

    Actively pulsed dual heating in vaporizing liquid microthrusters: an integrated analysis combining numerical simulations and experiments.

    12

    confirmed

    Ms. Angelica Maria Toscano

    Università del Salento

    Italy

    10

    16:48

    development of a 3d-printed cold gas propulsion system for cubesats

    12

    confirmed

    Mr. Victor Joseph Ochave

    Philippine Space Agency

    The Philippines

    11

    17:00

    Fuel Characterization, Performance Assessment and Thermal Analysis of a Hydrogen Peroxide-based Hybrid Thruster for CubeSats

    12

    confirmed

    Mr. Riccardo Guida

    Scuola Superiore Meridionale

    Italy

    12

    17:12

    Performance analysis of different air intakes for ABEP in VLEO and evaluation of scale effects

    12

    confirmed

    Mr. Antonio Sannino

    Università degli studi di Napoli Federico II, Dipartimento di Ingeneria Aerospaziale

    Italy