Abstract:
In recent years, air-breathing electric propulsion (ABEP) for very low Earth orbit (VLEO) has become a prominent research focus. ABEP systems utilize intake devices to collect atmospheric particles
in situ; these particles are ionized and accelerated by electric propulsion to generate thrust. Despite its potential, ABEP faces substantial engineering challenges. The VLEO atmospheric environment, the global development status of ABEP satellites, and recent advancements in intake device design are reviewed in this paper. A comparative analysis of electric thrusters using nitrogen-oxygen propellants is presented. Moreover, ten critical ABEP technologies – including system configuration, material selection, and ground-based simulation – are identified. Finally, key future research directions are outlined.