本文论述了固体火箭发动机燃烧室一维两相常滞后流动。
In this paper, one-dimensional two-phase constant lag flow in combustion chamber of solid propellant rocket motors is described.
介绍一种固体火箭发动机燃烧室壳体纤维缠绕芯模的设计。
This article introduces a designing means of mold of the fibre winding solid rocket motor combustion chamber shell.
认识到建立固体火箭发动机燃烧室X射线探伤像质计标准势在必行。
It was considered that the establishment of radiographic IQI standard for solid rocket motor chamber was necessary.
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