2) air-breathing propulsion
吸气推进
4) air feed
气力推进
6) liquefied gas propulsion
液化气推进
1.
A one-dimensional,heterogeneous liquefied gas self-pressurization computer model was developed based on mass and energy conservation equations to study performance of liquefied gas propulsion systems for small spacecrafts.
为研究小型航天器液化气推进系统的工作性能,依据质量、能量守恒方程建立了一维、单组元液化气自蒸发过程的数值模型。
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条