【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。更多还原

【Abstract】 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.更多还原