8-B4.5A. Joint Session between IAA and IAF for Small Satellite Propulsion Systems

Papers

1. Design of CubeSat propulsion system using hydrogen peroxide monopropellant thruster

2. MIMPS-G: Modular Impulsive Green-Monopropellant Propulsion System for Micro/Nano Satellites High-thrust demanding Orbital Maneuvers.

3. Test campaign of a Cubesat equipped with an helicon plasma thruster

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

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

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

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

11. Flow regime characterization of a MEMS-based vaporizing liquid microthruster

12. Sulfur-fueled Surface Arc Thruster for Propelling Nanosatellites

13. Initial Modelling of Cubesat Constellation Dispersal, Comparing Diverse Propulsion Technologies