ONE METHOD OF DETERMINING THE CRITERION OF OPERATIONAL STABILITY OF A LIQUID0-PROPELLANT ROCKET ENGINE

摘要

At the present time the methods for determining the conditions under which the operation of a liquid-propellant rocket engine (LRE) is stable are still not reliable enough. In the published literature the stability regions are determined graphically.nIn this article an attempt is made to find a certain new criterion which will allow analytical Investigation of the operational stability of LRE.