A power-plant parametric vector view build-up in the system of training-combat airplane during the preliminary stages of design is offered. In basis of a technique the mathematical simulation of an aircraft power-plant subsystem during all of life cycle is used by the means of heuristic methods, retrospective methods and experimental data. The reasoning of flying-technical and field-performance data of an aircraft is conducted by research of a standard flight cycle for an training airplane, trainingcombat or light combat airplane, that supposes the use of mathematical models of airplane flight, working process and life cycle of an aircraft power-plant sustainer engine in the system of an aircraft.
training-combat airplane, light combat airplane, aircraft, index, aircraft engine, power-plant, parametric vector view, cost of the life cycle of an aircraft engine, techno-economic efficiency, preliminary stage of design
"Metodyka formuvannia parametrychnoho obrysu sylovoi ustanovky v systemi navchalno-boiovoho litaka na poperednikh etapakh proektuvannia" ,
Science and Technology of the Air Force of Ukraine,