1) initial firing
首次的发射(火)
2) first open fire range
首次发射距离
1.
Through appropriate simplifying,3 main factors impacting kill effectiveness,such as the first open fire range(FOFR),kill probability and allocating target mode,are concretely analyzed in the paper.
通过适当的简化,文中具体分析了影响防空导弹系统在首发杀伤效能的3个主要因素:防空导弹首次发射距离、单枚导弹杀伤概率和目标分配方式。
3) initial firing
首次试验发射
5) the first flame
首次火焰
1.
Based on mathematic and physical meanings of the curves, the first flame time of sustaining grain was deduced as zero time of rise stage for pressure-rise velocity and the end time of flame propagation as the limit time from rise to drop.
为了定量描述大长径比固体火箭发动机点火滞后期和火焰传播过程,分析了试验压强 时间曲线和升压速率曲线,并利用数值计算对点火瞬态过程进行仿真;根据两条曲线的数学与物理意义推断主装药首次火焰时刻为升压速率上升阶段过零时刻,火焰传播结束时刻为升压速率由上升转下降的极值时刻;数值仿真结果验证了这一推断。
6) first fire
首次点火
1.
Based on the adiabatic approximation theory,we obtain the approximate expressions of the firing rate (FR),the probability distribution of the first fire (FPD),and the coefficient of variation (CV) of interspike interval of firing.
基于绝热近似理论,得到了神经元首次点火概率分布、神经元点火率和神经元点火峰峰间隔的变差系数的近似表达式。
补充资料：导弹机动发射(见导弹发射方式)
导弹机动发射(见导弹发射方式)
maneuverable launching of missile
算薰;笙簌巍骂 able launching 式。
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