The structure and performance parameters of typical monolithic non-intrinsic silicon IR focal plane array are presented.
介绍典型单片式非本征硅红外焦平面阵列的结构及性能参数。
The optimum results showed that some laws of the strain energy of the spring in clutch engaging and disengaging change with structure and performance parameters of the spring.
优化结果表明，弹簧在离合器接合和分离过程中的变形能随其结构参数和性能参数有某种变化规律。
Through adjusting the above structure and performance parameters, rational flight parameters can be decided, which can ensure the safe helicopter mission operations of the slung-load flight.
通过对上述结构参数、性能参数的调节，可确定合理、经济的飞行参数，保证安全、高效的完成直升机机外吊挂飞行运输任务。
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