pasty propellant rocket

基本解釋

The pasty propellant flame temperature measurement is very important to the propellant formula development and rocket motor design.
膏體推進劑火焰溫度測量對推進劑配方的研制及火箭發(fā)動機的設(shè)計具有重要意義。
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Research work in this dissertation has guiding significance for the design of pasty propellant rocket engine, and provides reference basis for pasty propellant striking from theory to application.
本文研究工作對膏體推進劑火箭發(fā)動機設(shè)計具一定的指導意義，為膏體推進劑火箭發(fā)動機從理論研究走向應(yīng)用提供了參考依據(jù)。