rootbrowseIAC-22C4session 8-B4.5A8-B4.5A. Joint Session between IAA and IAF for Small Satellite Propulsion SystemsPapers1. Development Status of Mono-Propulsion System for Active Debris Removal2. Development Status of Mono-Propulsion System for Active Debris Removal3. End-Of-Life Disposal of Sub-3U CubeSat with a printed thin-film Vacuum Arc Thruster4. Optimized vaporization in liquid-fed microresistojets using pulsed heating5. A study on solar sailing for low-power orbit-attitude control of small satellites in LEO6. A compact and high thrust-to-power micropropulsion system using ultrasonic vibrating mesh technology for PocketQube applications7. Environmental test campaign of a 12U CubeSat Test Platform equipped with an Ambipolar Plasma Thruster8. Development and testing of an engineering model of a hydrogen peroxide based 1N propulsion unit.9. experimental characterization of a hydrogen peroxide-based thruster for small satellites11. Space Mobility Optimization and Concurrent Engineering for Modular Micro-Propulsion Systems with 360 by ienai SPACE12. Leak Testing Procedure for Student-Designed Nanosatellite Propulsion/Feed Systems13. Flight results of the PETRUS pulsed plasma thruster on the 3u CubeSat GreenCube