Ignite the rocket thrust 点燃火箭产生推力
rocket thrust-chamber firing 火箭发动机点火试验
rocket-thrust-chamber nozzle 火箭推力室喷管
rocket thrust vector control 火箭推力矢量控制
rocket thrust line 火箭发动机推力线
rocket thrust chamber 火箭推力室
rocket thrust direction 火箭推力方向
Rocket thrust test bed 火箭推力试验台
A new calculation method was proposed for the typical structure of the platelet transpiration flux in the rocket thrust chamber based on the test data of another chamber.
针对典型的层板发汗冷却结构,提出了利用一个推力室的实验数据来计算另一推力室所需发汗流强的方法。
A piezoelectricity measuring system used for measuring rocket thrust vector is introduced. A devices to static accomplish, calibration and dynamic calibration on the system is designed.
重点介绍了一种用于测量火箭发动机推力矢量的压电式测试系统,并设计了对测试系统进行静态标定和动态标定的装置。
How can a rocket engine that generates 5,000 degree steam and 13,800 pounds of thrust form icicles at the rim of its nozzle?
一个能制造出5000度高温蒸汽和13800磅推力的火箭推进器,是怎样使喷口边缘结冰的呢?
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