等离子火箭是利用原子的猛烈撞击,使原子外层的电子外脱离原子核飞出来,成为带电的离子,用高压电场将这些离子加速到每小时15万公里的速度,高速离子流从喷口喷出,推动火箭前进。这也是一种小功率的火箭。
“等离子火箭能够做到持续加速”,他解释道。
"In a plasma rocket you're continually accelerating," he explains.
火箭探空实验观测结果显示,极区夏季中层顶尘埃等离子体分层中存在着稳定的锐边界结构。
The rocket experimental data indicated that the layered dusty plasma structure has a sharp boundary in the summer polar mesopause.
以轴对称非定常欧拉方程为基础,建立了激光推进火箭发动机吸收室内纯气相单组分、以激光等离子体为内热源的流场模型。
A gas flow model with laser plasma as heat source was developed based on axial symmetric Euler equations in the laser propulsion rocket engine absorption chamber.
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