CAJ | 학술논문

综述了固体推进剂的静态燃速、动态燃速和特定环境下的燃烧测试技术的研究现状以及各种燃速测试方法的特点，分析认为固体推进剂燃速测试技术的总体发展规律是由静态燃速测试逐步发展到动态燃速测试，在动态燃速测试的基础上出现了旋转过载燃速测试技术和压强瞬变条件下的燃速测试技术。现有燃速测试技术还用于测试固体推进剂常用高能添加剂的燃烧性能。提出了固体推进剂燃烧性能测试技术的发展方向：高压（超高压）燃烧性能测试技术、超低压（真空）燃烧性能测试技术、低温微重力环境下的燃烧性能测试技术等。附参考文献55篇。
종술료고체추진제적정태연속、동태연속화특정배경하적연소측시기술적연구현상이급각충연속측시방법적특점，분석인위고체추진제연속측시기술적총체발전규률시유정태연속측시축보발전도동태연속측시，재동태연속측시적기출상출현료선전과재연속측시기술화압강순변조건하적연속측시기술。현유연속측시기술환용우측시고체추진제상용고능첨가제적연소성능。제출료고체추진제연소성능측시기술적발전방향：고압（초고압）연소성능측시기술、초저압（진공）연소성능측시기술、저온미중력배경하적연소성능측시기술등。부삼고문헌55편。
The current research situation of static burning rate,dynamic burning rate and measurement technology of burning rate under specific environment for solid propellant,and characteristics of various burning rate measure-ment methods were reviewed.Considering that the general development rule of solid propellant burning rate meas-urement technology is that from the static burning rate measurement gradually developed into the dynamic burning rate measurement.On the basis of the dynamic burning rate measurement,the rotating overload burning rate meas-urement technology and burning rate measurement technology under the transient pressure condition appeared.The existing burning rate measurement technology is also used to test the combustion performance of commonly used high-energy additives in solid propellant.The future development direction of the combustion performance testing technology of solid propellant,including high pressure (ultra pressure)combustion performance measurement tech-nology,ultra low pressure (vacuum,)combustion performance measurement technology and low temperature micro-gravity combustion performance measurement technology etc,is pointed out with 55 references.