| タイトル | Measuring Response Of Propellant To Oscillatory Heat Flux |
| 著者（英） | Burns, Shawn P.; Strand, Leon D.; Schwartz, Ken |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1990-10-01 |
| 言語 | eng |
| 内容記述 | Apparatus for research in combustion of solid propellants measures oscillatory response of rate of burning to oscillating thermal radiation from modulated CO2 laser. Determines response to rate of burning to equivalent oscillation in pressure. Rod of propellant mounted in burner assembly including waveguide at one end and infrared window at other end. Microwave Doppler velocimeter measures motion of combustion front. Microwave, laser-current, and heat-flux signals processed into and recorded in forms useful in determining desired response of propellent. |
| NASA分類 | PHYSICAL SCIENCES |
| レポートNO | 90B10525
NPO-17428 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/360586 |
|
