1) time of flight of projectile; time of flight of bullet
弹头飞行时间
2) shell flight-time
射弹飞行时间
1.
On the basis of fitting the shell flight-time of anti-aircraft gun by integral exponential,this paper researches into the problem on changing the exponents of the parameter.
在高炮射弹飞行时间整数次幂拟合研究的基础上,用修改参数幂的次数的方法对拟合问题进行了研究。
2.
This paper researchs into the problem on fitting the shell flight-time of anti-aircraft gun by interpolation and quadratic approximation.
用插值拟合和最小二乘逼近拟合方法对高炮射弹飞行时间拟合问题进行了研究。
3) projectile flight time
弹丸飞行时间
1.
This paper presents an algorithm for finding projectile flight time with ensured acccuracy by solving the trajectory equations with unknown angle of departure only one time.
提出一种在保证一定计算精度的前提下，只解一次弹道方程组就可求得未知射角情况下目标点相应弹丸飞行时间的算法，而不需要在先求得准确射角后再解一次弹道方程组求解。
4) preset missile flight time
装定的导弹飞行时间
5) Flight time
飞行时间
1.
To design the interception guidance with the terminal aspect angle constraint,based on the formula given by other persons,a new solution was brought out,which main idea was to obtain the needed velocity vector by iterating the flight time;then modify the practical velocity during the flight time until the needed and the practical velocities are almost equivalent.
针对终点处交会角固定的拦截导引问题,基于前人得到的需用速度公式,提出了通过迭代飞行时间来确定能满足交会角要求的需用速度,并在飞行过程中不断修正实际速度使其与需用速度一致的方法。
2.
Two kinds of methods of determinating the explosion height through flight time are discussed in this paper,and one is the analytic computation and compensation method,while the other is the time partial derivative method.
分别讨论了两种通过飞行时间确定爆高的方法:解析计算修正法和时间偏导数法,这两种方法都是通过计算延迟时间来确定爆高,具有自主性强、可靠性高的特点。
3.
So,it is important for ballistic missile s firepower control to confirm shot time based on flight time.
为了达到最佳射击效果,弹道导弹突击目标时经常需要多枚导弹同时击中目标,因此根据飞行时间确定发射时间则成为弹道导弹火力控制问题的重要内容。
6) flying time
飞行时间
1.
The Measuring System for the Bullet s Flying Time and Falling Velocity;
弹丸飞行时间和落速测试系统
2.
Based on the analysis of the effect of liquor density on the muzzle velocity of spray droplets,the equation of the upward flying time of spray droplets in spray dryer was derived by Newton Second Law.
本文在分析料液密度对喷雾初速度影响的基础上,利用牛顿第二运动定律推导出雾滴向上飞行时间的计算公式。
3.
including ac- curacy of angle,acting range,and flying time.
文中针对运动爆炸目标测量系统,就高帧频电视对其测角精度、作用距离以及飞行时间等主要技术指标的影响做出了较全面的分析,并给出了指标估算方法。
补充资料：弹头气动加热(见弹头防热)
弹头气动加热(见弹头防热)
aerodynamic heating of warhead
dantou qidong iiare弹头气动加热(aerodynam，c heating。fWarhead)见弹头防热。
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