Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 45-49 |
| Number of pages | 5 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 20 |
| Issue number | 3 |
| State | Published - Mar 1999 |