摘要
An identification technique was presented for estimating the impurity level in propellant and the properties of exhaust afterburning, which can not be measured simply by experiment. The results of microwave attenuation calculated with the values of these parameters identified accord well with the experimental results. The identification results were also analyzed. It proved that this method is feasible in the study of microwave attenuation characteristics.
源语言 | 英语 |
---|---|
页(从-至) | 45-49 |
页数 | 5 |
期刊 | Tuijin Jishu/Journal of Propulsion Technology |
卷 | 20 |
期 | 3 |
出版状态 | 已出版 - 3月 1999 |