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  • 8-B4.5A
  • session 8-B4.5A

    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 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.

    Date

    2026-10-08

    Time

    15:00

    Room

    E6

    IPC members
    • Co-Chair: Mr. Jeffrey Michlitsch, The Aerospace Corporation, United States;

    • Co-Chair: Prof. Paolo Gessini, Brazilian Space Agency (AEB), Brazil;

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

    • Rapporteur: Prof. Sabrina Corpino, Politecnico di Torino, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    15:00

    A cost-effective, scalable thrust measurement system for a Solar Thermal Thruster prototype

    10

    confirmed

    Mr. Leonardo Dall'Osto

    Delft University of Technology (TU Delft)

    Netherlands (Kingdom of the)

    3

    15:10

    Calibration Methodology for a Micro-Newton Pendulum Thrust Balance Applied to Pulsed Plasma Thrusters

    10

    confirmed

    Ms. Ana Pereira

    University of Brasilia

    Brazil

    4

    15:20

    Conceptual Design of a Compact-COTS based Propulsion Module for CubeSat Applications

    10

    confirmed

    Dr. Soufyane Hazel

    Agence Spatiale Algérienne (ASAL)

    Algeria

    5

    15:30

    DESIGN OF A REGULATOR-LESS PROPELLANT FEED SYSTEM WITH ACTIVE THROTTLING CAPABILITIES FOR HALL THRUSTERS

    10

    confirmed

    Mr. Hidir Ilyas Sezer

    Istanbul Technical University

    Türkiye

    6

    15:40

    Development of Dual Mode Thruster for 2U-size Microsatellite-Friendly Multi-Purpose Propulsion System (MFMP-PROP) for Collision Avoidance Maneuver (CAM) and Post Mission Disposal (PMD)

    10

    confirmed

    Dr. Toshiaki Iizuka

    National Institute of Technology, Oyama College

    Japan

    7

    15:50

    High-Performance Cold-Gas Propulsion Module for 6U CubeSats: A Design and Simulation Case Study for Emerging Space Nations

    10

    confirmed

    Mr. GodsFavour Idaewor

    Nigeria

    8

    16:00

    Hybrid Rocket Propulsion System Integrated Aluminium-HTPB/N2O and Electric Propulsion

    10

    confirmed

    Mr. Kaustubh Singh

    Vellore Institute of Technology

    India

    9

    16:10

    Optimization of a hybrid chemical–electrical architecture for LEO–GEO transfer in small satellites

    10

    confirmed

    Mr. Carlos Gala

    Mexico

    10

    16:20

    Reusable Multi-Metallic Oxide Catalysts for Small Space Thrusters: regeneration after firing shots

    10

    confirmed

    Mr. Sergio Cassese

    University of Naples "Federico II"

    Italy

    11

    16:30

    Spectral Photon-Counting Computed Tomography for Non-Destructive Assessment of High-Precision Micro-Propulsion Systems

    10

    confirmed

    Dr. Djamal DARFILAL

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    12

    16:40

    Development of an Active Cooling System Using Water Propellant for Electric Thrusters in Micro-Satellites

    10

    confirmed

    Mr. Masaki Fujii

    The University of TOKYO, Graduate school

    Japan

    13

    16:50

    Thrust and Trust: The Regulatory Push for Sustainable Small Satellites

    10

    confirmed

    Ms. Miraslava Kazlouskaya

    ION-X

    France

    14

    17:00

    Estimation-Oriented Control Design for Real-Time Thrust Reconstruction in a Six-Degree-of-Freedom Null-Balance Thrust Stand

    10

    Mr. Keisuke Yorita

    The University of TOKYO, Graduate school

    Japan