rootbrowseIAC-17C4session 66. New Missions Enabled by New Propulsion Technology and SystemsPapers1. Using linear electromagnetic acceleration of satellite payloads for targeted atmospheric injection and orbital trajectory adjustment2. Application for Spacecraft in Very Low Orbits Based on Air-Breathing Electric Propulsion System3. Design and Development of a Sublimating Solid Propellant Tank for CubeSat and PocketQube Applications4. Electrodynamic wing for LEO spacecraft propulsion5. SYSTEM ANALYSIS AND TEST-BED FOR AN ATMOSPHERE-BREATHING ELECTRIC PROPULSION SYSTEM USING AN INDUCTIVE PLASMA THRUSTER6. Feasibility of an Integrated Solar Thermal Power and Propulsion System for Small Satellites7. Electric propulsion for high-power deep space transportation system: investigation on mutual influences and preliminary sizing8. Stationkeeping with an electrospray propulsion system for low lunar polar mission on a 6U CubeSat9. Unique Advantages of Hybrid Rocket Technology for Mars Missions10. Finding NewSpace: Mission Scenarios Utilizing LOTUS: Lander/Orbiter Trans-Upper Stage11. Overview and Analysis of Msail and Esail Propulsion for Interplanetary Misions12. Increasing the Accuracy of Electric Sail Mission Performance Estimates