Abstract The mathematical model and research results of processes running in the interconnected system of “solid propellant propulsion system—swiveling controlled nozzle—flexible joint—gas-hydraulic actuator” are represented. The possibility of increasing the aircraft efficiency due to the inherent features of the system under study is shown.
Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
Russian Aeronautics ; 62 , 2 ; 222-228
2019-04-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch