rootbrowseIAC-17C4session 8-B4.5A8-B4.5A. Joint Session between IAA and IAF for Small Satellite Propulsion SystemsPapers1. KEYNOTE: Progress and challenges of small satellite propulsion systems2. The Pocket Rocket electro-thermal plasma thruster for ‘CubeSat’ nano-satellites3. A low-cost Helicon Propulsion System to boost small satellite missions.4. mems based micro-propulsion system for cubesats and pocketqubes5. HET based propulsion system onboard the µHETsat mission6. Advancements in High-Performance Green SmallSat/CubeSat Propulsion7. Recent development of Hydroxylammonium Nitrate (HAN) green liquid monopropellant in Malaysia8. Design and Testing of a Hybrid Rocket Motor to Enable Interplanetary CubeSat Missions9. Multi-variable Optimization of Gaseous Oxygen Hybrid Rocket Motors for Small Satellite Propulsion10. development of gap/ap solid propulsion system for ultra-small satellite11. Environment and Qualification Test Results of the Highly Miniaturized FEEP Propulsion System NanoFEEP12. Development of a Launch Safe CubeSat and Microsatellite Water Propulsion System13. Design of a Flexible Propulsion Testbed for Cubesats14. self-pressurized small-satellite propulsion system using supercritical phase transition15. Design and Testing of A Modular, Cold Gas Propulsion System for Small Satellite Applications