1) Two stage to orbit vehicle
两级入轨飞行器
2) Single stage to orbit vehicle
单级入轨飞行器
3) two-stage-to-orbit
两级入轨
1.
From the capability analysis of the single-stage-to-orbit and two-stage-to-orbit,the paper combines the actual condition of the Chinese aerospace,puts forward a kind of development path to develop the two-stage-to-orbit reusable launch vehicle based on the expendable launch vehicle,and suggests a scheme of small reusable launch vehicle of two-stage-to-orbit.
从分析单级入轨和两级入轨的运载性能出发,结合中国航天实际条件,提出研制以一次性使用运载火箭为基础的两级入轨的重复使用运载器的发展途径,并提出一种小型两级入轨重复使用运载器的方案设想。
4) orbit vehicle
在轨飞行器
1.
The effect of the orbital drift on the image of a orbit vehicle is analyzed.
分析了在轨飞行器轨道漂移对目标成像位置的影响,以及由此产生的目标定位误差;利用已知地标的成像位置,可以确定轨道漂移的量,从而对目标图像进行补偿修正,提高目标定位精度。
6) reentry vehicle
再入飞行器
1.
Aerodynamics prediction and configuration optimizati on for reentry vehicle with double-ellipse cross-section;
双椭圆截面再入飞行器的气动计算及布局优化设计
2.
Fluctuating response analysis of reentry vehicles;
再入飞行器的脉动响应分析
3.
Unscented Kalman Filtering for Reentry Vehicle Tracking;
Unscented Kalman滤波用于再入飞行器跟踪
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