一种适用于超低轨道卫星的吸气式喷射推进装置
By employing a combination of a gas selective separation supply structure and a Hall-like thruster on ultra-low orbit satellites, the problem of oxygen damage to electrodes has been solved, gas utilization efficiency has been improved, and costs have been reduced, thus meeting the requirements of green aviation.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- INST OF MECHANICS CHINESE ACAD OF SCI
- Filing Date
- 2024-02-05
- Publication Date
- 2026-07-17
AI Technical Summary
Existing ultra-low orbit air-breathing electric propulsion technology suffers from low efficiency and high cost when utilizing rarefied gases, as the oxygen content in the gas can damage components such as electrodes and neutralizers, making it difficult to meet the requirements of green aviation.
The gas selective separation supply structure is adopted to separate the inhaled gas into components and supply them to different gas supply channels through the ionization zone in the Hall thruster, avoiding direct contact between oxygen components and electrodes. Combined with the gas enrichment and transfer unit and the separation supply unit, the gas is separated and recombined by temperature and pressure differences, thereby improving utilization efficiency.
It effectively avoids component damage, improves gas utilization efficiency, reduces operating costs, and achieves efficient utilization of environmental gases.
Smart Images
Figure CN117842390B_ABST