1) Attitude and orbit control thruster
姿/轨控液体发动机
2) solid rocket divert and attitude control motor
固体姿轨控发动机
1.
The fast driving circuit for gas solenoid valve of solid rocket divert and attitude control motor;
固体姿轨控发动机燃气电磁阀快速驱动电路研究
3) attitude-control and orbit-control engines
姿控轨控发动机
4) attitude control engine
姿控发动机
1.
Research on outlet pressure deviation calculation of pressure reducing valve for attitude control engine;
姿控发动机减压阀出口压力偏差计算方法研究
2.
The side jet technology of foreign advanced surface-to-air missiles is analyzed,disperse thrust models of 180 attitude control engines of patriot-III missile is built,and some optimized methods of ignite technology is studied,then the result of the simulation is presented.
跟踪与分析国外先进防空导弹的姿控发动机控制技术,以美国PAC-3导弹为例,对姿控发动机组建立离散模型,然后采用一定的优化方法,对其点火方法作了研究,并提供仿真结果。
3.
Using the plentiful software and USB interface of PC,taking FPGA as the core,controling the correspondence of the chip of USB,the automatic test of multi-pulse attitude control engine system status and the ignition of multi-pulse attitude control engines were carried out in this paper.
利用PC丰富的软件和USB接口,以FPGA为核心,控制USB芯片的通信,实现了多脉冲姿控发动机系统状态的自动检测和多脉冲姿控发动机的点火。
5) side jet
姿控发动机
1.
In missiles using direct force control systems, a high precision robust guidance law with low side jet consuming is required.
最后进行了三维弹道仿真,结果表明:所设计的导引律攻击精度明显优于比例导引律,尤其是在目标机动较大情况下,保证了脱靶量在米级以内;所设计的导引律在制导初期对误差进行修正,因而末端弹道更为平直,同情况下所消耗的姿控发动机数目更少。
2.
In this paper, an attitude control method using side jets of a kind of long-distance air defense missile is studied.
以某型远程地空导弹为背景,研究了以姿控发动机作为执行机构下导弹的姿态控制问题。
6) attitude control thruster
姿控发动机
1.
Experimental study on plume impingement effects of satellite attitude control thruster nozzle;
卫星姿控发动机喷管羽流撞击效应试验
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
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