Structural and technological methods on ensuring of flight suitability of military non-combat aircraft air fame

Authors
DOI:
https://doi.org/10.34169/2414-0651.2019.2(22).67-77
Keywords:
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Abstract

The constructive-technological methods of ensuring the airworthiness of the airliner airliner are analyzed, with the aim of preserving the competitiveness of domestic aircraft construction in the world market for aviation and transport services.

Author Biographies
  1. I. B. Chepkov, Central Scientific Research Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Doctor of Engineering
    professor
    Chief C.S.R.I.A.M.E.A.F.U.

  2. Valeriy Zubariev, Central Scientific Research Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Doctor of science, professor

    Principal researcher of the group of Principal researcher of scientific research guidance Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Kyiv, Ukraine

  3. O. O. Holovin, Central Scientific Research Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Candidate of Technical Sciences
    Senior Research Fellow
    Chief of the Research Directorate for the Development of Arms and Military Equipment of the Air Force

  4. G. O. Krivov, Ukrainian Research Aviation Institute technologies

    Doctor of Engineering
    professor

  5. O. G. Hrebenikov, National Aerospace University named after. M.J. Zhukovsky "Kharkiv Aviation institute"

    Doctor of Engineering
    professor

References
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Published
2019-06-16
Issue
Vol. 22 No. 2 (2019): Weapons and military equipment
Section
AIRCRAFT ARMAMENT & FACILITIES
License
Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

Structural and technological methods on ensuring of flight suitability of military non-combat aircraft air fame. (2019). Weapons and Military Equipment, 22(2), 67-77. https://doi.org/10.34169/2414-0651.2019.2(22).67-77

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