"In a plasma rocket you're continually accelerating," he explains.
“等离子火箭能够做到持续加速”，他解释道。
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.
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。
His rocket harnesses a nuclear process to produce a hot gas plasma.
他设计的火箭能利用核反应过程产生的一种高温的气态等离子体。
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