1) Thermal protection system
防热系统
1.
Health Monitoring for Thermal Protection Systems on Reusable Launch Vehicles;
重复使用跨大气层飞行器防热系统健康监控技术研究
2.
With the development of reusable launch vehicles, the thermal protection system has been oriented by the idea of incorporate design which involves thermal protection - structure - thrust system.
随着可重复使用航天器的发展,热防护系统在向着防热-结构-推进系统一体化设计的方向发展,与此同时,整个防热系统在总起飞重量中所占的重量比例也在降低,而使用温度升高,即要求防热结构日趋先进。
3.
With the development of reusable launch vehicles, thermal protection system has been oriented by the idea of incorporate design which involves thermal protection - structure - thrust system.
随着可重复使用航天器的发展,热防护系统向着防热-结构-推进系统一体化设计的方向发展,与此同时,整个防热系统在总起飞重量中所占的重量比例也在降低,而使用温度升高,即要求防热结构日趋先进。
2) thermal protection system
热防护系统
1.
This paper mainly introduces the application research progress of CFRCMCs in thermal protection system,rocket engine and scramjet.
主要介绍了国外CFRCMCs在热防护系统、火箭发动机和超燃冲压发动机上应用的研究进展。
2.
The combined radiation /conduction heat transfer in thermal protection systems(TPSes)for reusable launch vehicles was analyzed using the APDL language of ANSYS to simulate reentry aerodynamic heating conditions.
针对可重复使用飞行器再入过程中热防护系统的复杂辐射-传导传热问题,采用有限元方法并结合仿真软件ANSYS的参数化分析语言APDL,对可重复使用飞行器热防护系统进行参数化求解,模拟再入条件下热防护系统内部辐射和传导复合换热,预测内部瞬态温度响应。
3.
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。
3) thermal antifouling system(TAS)
热防污系统
1.
The article briefly introduces the box cooler and thermal antifouling system(TAS)with their application in the 6800 DWT MPV.
结合6800t多用途船的实例对箱式冷却器在现代船舶中的使用情况作简单介绍,并对热防污系统(TAS)的应用作简要推介。
4) Thermal protection system(TPS)
热防护系统
1.
The unique function of the thermal protection system(TPS) is to maintain the vehicle structural temperature within allowable limit during re-entry aerodynamic heating, which is critical to a new generation of reusable launch vehicles(RLV).
先进热防护系统(TPS)的设计是决定可重复使用运载器(RLV)成败的关键技术之一。
5) THERMAL ANTI-ICING SYSTEMS
热防冰系统
6) TPS
热防护系统
1.
Such aircrafts suffer extremely thermal environment during flight, so the forecast of aerodynamic heating and thermal protection system (TPS) design is one of the key technologies of hypersonic vehicle design and manufacture.
由于高速飞行器的气动加热与热防护系统的热响应是耦合的,通过数值方法进行气动热与热结构的耦合分析,需要对飞行器进行整体建模分析,涉及高温空气的化学非平衡边界层传热,湍流模型和复杂结构传热模型,需要耗费大量的计算机资源和时间;采用风洞进行试验且不说耗费惊人的人力和财力,仅建造能模拟马赫数10以上的飞行条件的风洞就是一个巨大的挑战。
2.
It can simulate not only the thermal /pressure condition subjected by the outer surface of TPS but also the vacuum pressure subjected by the inner surface of TPS.
介绍了一种能模拟可重复使用运载器热防护系统内、外表面气动热和压力环境的热真空模拟试验装置,该装置不仅能模拟TPS外表面所受气动热和气动压力条件,还能模拟TPS内表面的真空压力环境。
补充资料：弹头烧蚀(见弹头防热)
弹头烧蚀(见弹头防热)
warhead ablation
dantou shaoshi弹头烧蚀(warhead的lation)见弹头防热。
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