摘要

Air-breathing electric propulsion is a very promising propulsion technology for ultra-low-orbit satellite, and one of the keys is to efficiently collect atmospheric molecules as propellant. Several representative air-intake systems are compared and analyzed, which helps to summarize the basic principles to increase collection efficiency. The common physical problems in air-intake systems are then investigated through theoretical analysis and numerical simulation, and the influence of key parameters such as non-dimensional tube length and exit transmission probability on collection efficiency is obtained. It is found that when the non-dimensional tube length increases the collection efficiency first increases and then decreases, and the highest collection efficiency shows a positive correlation with the exit transmission probability.Based on the analysis, a preliminary design of air-intake system is provided for earth orbit at 150 km and the optimized collection efficiency is over 50%.

全文