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Experimental Investigation of the Pressure Characteristics in Air-Breathing Laser Propulsion

机译:空气呼吸激光推进器压力特性的实验研究

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Keeping the single pulse energy of the CO{sub}2 laser constant, the impulse coupling coefficients of air-breathing laser propulsion are measured at various air pressures using a high precision impact pendulum system and the corresponding altitude characteristics. The results show that the impulse coupling coefficient is about 35dyne.s/J with less than 5% fluctuation when the air pressure varies from 2.8 × 10{sup}4 Pa to 1 × 10{sup}5 Pa and the altitude from Okm to 10km. When the air pressure is less than 2.8 × 10{sup}4 Pa and the altitude is greater than 10km, the impulse coupling coefficients decrease following a quadric curve. At a pressure of 1 × 10{sup}3 Pa and altitude of 31km, the impulse coupling coefficient is only 9.7dyne.s/J i.e. a drop of 75%. These results, which can be explained as due to the angle of the thrust, are consistent with those of German work using a parabolic device.
机译:保持CO {sub} 2激光的单脉冲能量恒定,使用高精度冲击摆系统和相应的高度特性,在各种气压下测量呼吸式激光推进器的脉冲耦合系数。结果表明,当气压从2.8×10 {sup} 4 Pa到1×10 {sup} 5 Pa且从Okm到10公里当气压小于2.8×10 {sup} 4 Pa并且高度大于10km时,脉冲耦合系数将按照二次曲线减小。在1×10 {sup} 3 Pa的压力和31km的高度下,脉冲耦合系数仅为9.7dyne.s / J,即下降了75%。这些结果可以用推力角度来解释,这与德国使用抛物线装置的研究结果一致。

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