Thermal control material OSR's have to meet a variety of ground and space environments during ground storage and space flight of space vehicles.
航天器在地面待发射期间加空间实际飞行过程中，热控元件OSR要遇到各种地面和空间环境。
The thermal stage separation being provided with improving and enhancing stability and orbit precision for flight was abroad adopted in solid-propellant ballistic missile.
级间热分离具有改善和提高继续飞行级的稳定性和入轨精度而被固体弹道式导弹广泛采用。
According to flight feature and transitional thermal load value, scheme of temperature adjusting system of electronic equipment cabin was presented.
根据高空高速飞行特点及瞬态热载荷值，确定仪器设备舱调温系统方案。
A baseline vehicle is presented for the given flight mission, and the effects of the tank material, the thermal protection system and the design margin on the vehicle dry mass are calculated.
对给定的飞行任务，提出了基准运载器，并计算了贮箱材料、热防护系统及设计余量对运载器干质量的影响。
Flight controllers initially thought it might be one of the shuttle's thermal blankets.
飞行控制器最初觉得它可能是航天飞机的隔热层的之一。
Using DSC-Coulometric Nitrogen Oxide Detector, Time of Flight Mass Spectrometer, the authors studied the thermal decomposition characteristics of HMX and its catalytic systems.
用DSC -库仑池联用仪和飞行时间质谱仪对HMX及其催化体系的热分解进行了研究。
The design analysis, tests and flight results of a local thermal-protection structure are introduced.
分析了防热结构的局部过热现象，提出了一种局部防热结构设计分析方法。
The design analysis, tests and flight results of a local thermal-protection structure are introduced.
分析了防热结构的局部过热现象，提出了一种局部防热结构设计分析方法。
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