释义 |
RBCC 基本例句 火箭苍组合动力循环¹⁰⁰ As for the research of the performance of the motor, the directedRBCCis adopted mostly.对于发动机性能的研究,国内外大多采用直连式RBCC实验系统进行研究。 The utilization of rocket ejector is important to structural integration ofRBCC, for it may decrease weight and complexity of the motor.利用引射火箭+试验系统和固体火箭发动机燃气发生器,就不同结构的二次喷管对引射火箭+的性能影响开展了试验和数值模拟研究。 For it s excellent performance, Rocket-Based-Combined-Cycle should be the most competitive propulsion system of Hypersonic Flight Vehicle for martial and civil purpose.RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。 RBCCis a most potential project of motor to realize the high super-sonic flight, and focuses great attentions for its extensive military and civilian astronautic application foreground.火箭基组合循环推进系统是实现高超声速飞行的最有潜力的动力方案,具有广泛的军事和民用航天应用前景,因而备受瞩目。 Rocket-Based-Combined-Cycle火箭基组合循环RBCC |