Space-Purpose Rockets Propulsion Systems Design Algorithm
Results of the space-purpose rockets propulsion systems design experiment-calculated method implementation during development work with "Angara" and "Oxygen-hydrogen upper-stage rocket KVTK" at M.V. Khrunichev State Research and Production Space Center's (SRPSC) "Salyut" design bureau are under consideration. It is noted, that the method's main peculiarities are the mathematical modeling application during the engine experimental development and the bench-top articles tests parameters definition as the basis to the next test phase transition.