The characterization of the combustion properties of the aluminum? Magnesium fuel? Rich propellant for unchoked ductedrocket was studied.
系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
2
The effects of various parameters on boron particle ignition of ductedrocket secondary chamber were studied with the model developed by the King.
硼颗粒在通过固体火箭冲压发动机的燃气发生器喷管进入补燃室的过程中，颗粒通常都会受到高速气流的作用。
3
The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ductedrocket are investigated.