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3. Intake design for an Atmosphere-Breathing Electric Propulsion System (ABEP)

4. In-orbit aerodynamic coefficient measurements using SOAR (Satellite for Orbital Aerodynamics Research)

5. RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)

6. System design study of a VLEO satellite platform using the IRS RF helicon-based plasma thruster

9. The benefits of very low earth orbit for earth observation missions

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