1) constant altitude flight
等高飞行
1.
The tentative design of constant altitude flight solid rocket composed of the sustainer ,the booster and its simple control method is presented.
介绍了主发动机加助推器和简易控制方法实现固体火箭等高飞行的设计方案。
2) equivalent flying
等效飞行
4) flight altitude
飞行高度
1.
Combined with the GJB and the characteristic of the environment control system of airplane, the ventilation and cooling condition of airborne electronic equipments in factual use environment was investigated;Combined with the life profile, task profile and its environment condition, flight altitude, flight mach number, etc, the stress in reliability test and the problems in those standards in.
结合国家军用标准和飞机环控系统的特点对机载电子设备实际使用中的通风冷却条件进行了研究,结合产品的寿命剖面、任务剖面,针对不同任务的环境条件、飞行高度和飞行马赫数等条件,对产品在可靠性试验中通风冷却应力的施加进行了探索性研究,对现行标准中存在的问题进行了对比研究,阐述了在可靠性试验过程中如何模拟其实际使用中的通风冷却条件,制定出合理、可行的通风冷却试验剖面(包括通风气体流量、温度、湿度和洁净度等参数的确定方法) 。
5) flying height
飞行高度
1.
A new structure of integrated optical flying head (OFH), with both perfect mechanical and optical performance, is designed, which can achieve stable flying height and high signal/noise ratio optical signal during the read/write motion in near field recording (NFR) system.
设计了一种新型一体化光学飞行头,通过对光学飞行头滑块气浮力分布和飞行姿态(飞行高度、仰俯角和滚动角)的数值仿真分析,对滑块气体轴承表面(ABS)形貌参数进行了优化设计,确定了滑块的主要结构参数。
2.
A dual wavelength multistep method for measuring flying height is constructed.
近场存储技术是近年来最具发展潜力的信息存储技术之一,微飞行头与存储介质间的飞行高度测试成为高密度存储的关键。
6) flight height
飞行高度
1.
A calculation method of bumping ground probability of the flight is presented and at the same time the calculation example of bumping ground probability in relation to flight height is also given in the paper.
研究了巡航导弹飞行高度控制系统对应的高度控制误差和地形起伏误差,在综合这两种误差的基础上,提供了一种飞行撞地概率的计算方法,并给出了飞行高度与之对应的撞地概率计算实例。
补充资料：复杂气象飞行(见飞行技术)
复杂气象飞行(见飞行技术)
instrument meteorological conditions flight
fuza qixiangfe主xing复杂气象飞行(instrument meteorologiealconditions flight)见飞行技术。
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