VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University698210.18287/2541-7533-2003-0-1 (3)-106-110DETERMINING GEOMETRICAL PARAMETERS OF CENTRIPETAL MICROTURBINE NOZZLE CONSISTING OF RECTILINEAR BLADESMussatkinN. F.vest@ssau.ruRadkoV. M.vest@ssau.ruBalakhonovA. D.vest@ssau.ruSamara State Aerospace University18032003211061102808201928082019Copyright © 2019, VESTNIK of Samara University. Aerospace and Mechanical Engineering2019<span>A procedure for determining structural geometrical parameters of nozzle blade profiles on the basis of the results of gas-dynamic calculation of a stage of a radial centripetal microturbine is presented.</span>