虚拟仪器技术在高压强及高燃速固体推进剂燃速测试中的应用  

The Application of Virtual Instruments to Burning Rate Measurement of High Pressure and High Burning Rate Solid Propellant

作　　者：刘宏成[1] 李葆萱[1] 李逢春[1] 

机构地区：[1]西北工业大学航天学院,西安710072

出　　处：《弹箭与制导学报》2005年第S4期385-387,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：描述了将虚拟仪器技术用于高压强、高燃速固体推进剂燃速测试系统的具体研究过程和结果。研究表明,该测试系统具有硬件配置简单、软件操作简便灵活、功能完善等优点。该研究成果对虚拟仪器技术在航天推进技术领域的应用和开发具有一定的参考价值。This paper expatiates the developing process,results and application of a system which is developed by use of virtual instrument technique.The system completes the measurement of the burning rate of the solid propellant in high pressure and that of the high burning rate solid propellant.This system comprises the simple hardware equipments and convenient software,possesses perfect functions,and provides some reference in the field of space propulsion technolo- gy using virtual instrument technique.

关 键 词：虚拟仪器 LABVIEW 固体推进剂 燃速测试 

分 类 号：V512[航空宇航科学与技术—航空宇航推进理论与工程]