Open Information and Computer Integrated Technologies

Development of perspective high-speed aircrafts inseparably linked with level of aircraft propulsion engineering as engine performances to determine aircraft capabilities as a whole. The basic requirements to engines of high-speed aircrafts are increase speed and flight height. With each new generation of turbojet bypass engine with afterburner their specific thrust and a specific impulse are increase, also application of high technologies raises leads to substantial growth of the engine cost too. At the same time existing engines design has the big reserves for modernization. For a quantitative assessment of the degree of influence of the new technical solution on the quality of the task performance by the aviation complex, criteria (indicators) of efficiency are used. However, it is not possible to find a direct functional dependence of the overall criterion of the effectiveness of the aviation complex on the technical and operational characteristics, conditions of use of a high-speed aircraft. The purpose of this work is to develop a methodology for determining the economic criterion for assessing the degree of influence of a new technical solution on the quality of the task performance by the aviation complex (the value of the integrated performance criterion). The text of the paper provides an analysis of recent research and publications. The developed relative criterion of the efficiency of a high-speed aircraft makes it possible to accomplish the goal set, as well as to estimate the costs at the cost of which the final result is achieved. It is shown that boosting engines with water injection has some advantage over other options for increasing the thrust of high-speed aircraft engines. The application of the obtained results can be used to substantiate new technical solutions and establish their impact on the quality of the task performance by the aviation complex, as well as reduce the time to create competitive high-speed aircraft.

Warwick Graham. Unmanned Combat Air Vehicles. Aviation Week & Space Technology, 29 December 2014 – 14 January 2015, New York, 2015, no. 47, pp. 95.

Norris Guy. Sonic QueSST. Aviation Week & Space Technology, 20 June – 3 July 2016, New York, 2016, no. 13, pp. 38-39.

Svitak Amy. A Turning Point in U.K. Space. Aviation Week & Space Technol-ogy, 4-17 July 2016, New York, 2016, no. 14, pp. 88-89.

McIntosh David. The Sky is not the limit. Farnborough Airshow News, Wednesday, 2016, London, 2016, pp. 8.

Kalinichenko, D. S., Aksjonenko, A. V., Kashanov, A. Je. Metodicheskij pod-hod k proektirovaniju transportno-kosmicheskoj sistemy [Methodical approach to the design of transport and space systems]. NAKU «KhAY» «Aviatsiyno-kosmichna tekhnika i tekhnolohiya» [Proc. of the Zhukovsky National Aero-space University «Kharkiv Aviation Institute» «Aviation and space technique and technology»], 2012, vol. 4(91), pp. 27–33.

Hadhazy Adam. Recycled Military Jets Serve as Satellite Launchers. Available at: http://www.space.com/9380-recycled-military-jets-serve-satellite-launchers (accessed 01.10.2010).

Makeich, G. S., Tjukaev, M. Ju., Chibisov, Ja. N. Proekt «Molot» giperzvu-kovogo bespilotnogo samoleta-razgonshhika s kombinirovannoj jekrannoj tur-boprjamotochnoj silovoj ustanovkoj [Project «Hammer» hypersonic pilotless aircraft responsice combined display Turboremont power plant]. Available at: http://www.mai.ru/science/trudy/published.php?ID=29075 (Accessed 2012).

Ambrozhevich M.V., Kartashev A.S., Jashin S.A. Kriterial'nye ocenki transportnogo sovershenstva letatel'nyh apparatov s ballisticheskimi i or-bital'nymi traektorijami poleta [Criteria estimations of the transport perfection of flying vehicles with ballistic and orbital flight paths]. NAKU «KhAY» «Avi-atsiyno-kosmichna tekhnika i tekhnolohiya» [Proc. of the Zhukovsky National Aerospace University «Kharkiv Aviation Institute» «Aviation and space tech-nique and technology»], 2006, vol. 4, pp. 25–30.

Ambrozhevich M.V., Kartashev A.S., Jashin S.A. Kriterial'nye ocenki jenerget-icheskogo sovershenstva atmosfernyh raketnyh letatel'nyh apparatov [Criteria for assessing the energy perfection of atmospheric rocket aircraft]. NAKU «KhAY» «Aviatsiyno-kosmichna tekhnika i tekhnolohiya» [Proc. of the Zhu-kovsky National Aerospace University «Kharkiv Aviation Institute» «Aviation and space technique and technology»], 2006, vol. 5, pp. 21–29.

Ambrozhevich M.V., Kartashev A.S., Jashin S.A. Kriterial'nye ocenki transportnogo i skorostnogo sovershenstva ajerodinamicheskih letatel'nyh apparatov [Criteria evaluation of the transport and speed perfection of aero-dynamic aircraft]. NAKU «KhAY» «Aviatsiyno-kosmichna tekhnika i tekhnolo-hiya» [Proc. of the Zhukovsky National Aerospace University «Kharkiv Avia-tion Institute» «Aviation and space technique and technology»], 2006, vol. 6, pp. 19–23.

Ambrozhevich M.V., Kartashev A.S., Sereda V.A. Kriterial'nye ocenki jenerget-icheskogo sovershenstva dvuhstupenchatyh bespilotnyh letatel'nyh appa-ratov [Criteria for assessing the energy perfection of two-stage unmanned aerial vehicles]. NAKU «KhAY» «Aviatsiyno-kosmichna tekhnika i tekhnolo-hiya» [Proc. of the Zhukovsky National Aerospace University «Kharkiv Avia-tion Institute» «Aviation and space technique and technology»], 2008, vol. 3, pp. 51–55.

Ambrozhevich M.V., Kartashev A.S., Sereda V.A. Kriterial'nye ocenki jenerget-icheskogo sovershenstva processa vyvedenija bespilotnyh letatel'nyh appa-ratov aerodromnogo starta [Criteria assessments of the energy perfection of the launching process of unmanned aerial vehicles of the aero-homing launch]. NAKU «KhAY» «Aviatsiyno-kosmichna tekhnika i tekhnolohiya» [Proc. of the Zhukovsky National Aerospace University «Kharkiv Aviation In-stitute» «Aviation and space technique and technology»], 2009, vol. 1, pp. 5–9.

Yelans`ky`j O.V. Ocinka doskonalosti aviacijnogo navchal`no-bojovogo kom-pleksu na poperednix etapax jogo proektuvannya abo podal`shoyi moderni-zaciyi [Assessment of the perfection of the aviation training complex at previ-ous stages of its design or further modernization]. KhUPS «Systemy ozbroy-ennya i viys'kova tekhnika» [of the Kozhedub Kharkiv University of Air Forse «Weapons systems and military equipment»], 2014, vol. 3, pp. 33–36.

Loginov V.V., Elanskij A.V., Kravchenko I.F. Metodologicheskie osnovy formi-rovanija parametricheskogo oblika silovoj ustanovki perspektivnogo uchebno-boevogo samoleta [Methodological basis for the formation of the parametric appearance of the power plant promising combat training aircraft]. Kharkiv, of the Kozhedub Kharkiv University of Air Forse Publ., 2016. 294 p.

Korochkin A.A., Suhanov I.M. Vzaimozavisimost' taktiko-tehnicheskih i jekonomicheskih ha-rakteristik BAK [Interdependence of technical and eco-nomic characteristics of the LHC]. Kharkiv, HVVAIU Publ., 1984. 40 p.