DEVELOPMENT OF THE TEST EQUIPMENT OF THE SUIT-5 SYSTEM ON AN-74 PLANE

The investigation of fuel flow system of the An-74 plane with the subsequent design of the wiring schematic scheme of the test and control equipment for serviceability check of the measurement and control system of the SUIT-5 propellant established on plane was the purpose of this work. The results of the development allowing to create the universal test equipment for use both in airfield, and in laboratory are presented in the work.