The malfunction of thermal protection system on reusable launch vehicle will generate a heat source on the part of vehicle.

可重复使用运载器的防热瓦故障会使航天器的局部结构产生热源，并在结构中形成温度场。

Many have called for NASA to develop a new reusable launch vehicle that will substantially reduce the cost of launch to orbit.

许多人呼吁美国太空总署研发一种新型的可回收发射载具，以便充分地压低发射器飞行成本。

Thermal protection system (TPS) is one of the key technologies for space vehicle, especially for reusable launch vehicles (RLV).

热防护系统是航天飞行器 ，特别是重复使用运载器的关键技术之一。

It is indicated that the metal lic TPS is the one of top priority blue prints of the acreage TPS for the next generation reusable launch vehicle.

指出金属热防护系统仍是下一代重复使用运载器大面积表面热防护系统的优选方案之一。

The objective of this paper is to design the reentry flight control laws for the Suborbital Reusable Launch Vehicle(SRLV) based on nonlinear dynamic-inversion.

基于非线性动态逆理论，设计了亚轨道可重复使用运载器（SRLV）的再入控制律。