摘要
介绍了用随机小尺寸试验发动机平均燃速预估全尺寸发动机燃速的方法,讨论了全尺寸发动机燃速预估精度及其影响因素,并通过实例指出提高全尺寸发动机燃速预估精度的主要途径。
A method to predict the burning rate of full-scale motor by the average burning rate of the accompanied sub-scale test motors was put forward. The factors which affect the prediction accuracy of the full-scale motor burning rate were discussed. And the principal approachs which can improve the accuracy of prediction were pointed out based on an example.
出处
《固体火箭技术》
EI
CAS
CSCD
1996年第4期36-40,共5页
Journal of Solid Rocket Technology
关键词
固体推进剂
火箭发动机
固体推进剂
燃速
Solid propellant rocket engine
Solid propellant
Engine test
Propellant burning rate