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  • session 6
  • 6. New Missions Enabled by New Propulsion Technology and Systems

    Papers

    1. Using linear electromagnetic acceleration of satellite payloads for targeted atmospheric injection and orbital trajectory adjustment

    2. Application for Spacecraft in Very Low Orbits Based on Air-Breathing Electric Propulsion System

    3. Design and Development of a Sublimating Solid Propellant Tank for CubeSat and PocketQube Applications

    4. Electrodynamic wing for LEO spacecraft propulsion

    5. SYSTEM ANALYSIS AND TEST-BED FOR AN ATMOSPHERE-BREATHING ELECTRIC PROPULSION SYSTEM USING AN INDUCTIVE PLASMA THRUSTER

    6. Feasibility of an Integrated Solar Thermal Power and Propulsion System for Small Satellites

    7. Electric propulsion for high-power deep space transportation system: investigation on mutual influences and preliminary sizing

    8. Stationkeeping with an electrospray propulsion system for low lunar polar mission on a 6U CubeSat

    9. Unique Advantages of Hybrid Rocket Technology for Mars Missions

    10. Finding NewSpace: Mission Scenarios Utilizing LOTUS: Lander/Orbiter Trans-Upper Stage

    11. Overview and Analysis of Msail and Esail Propulsion for Interplanetary Misions

    12. Increasing the Accuracy of Electric Sail Mission Performance Estimates