Method of calculating of the range of angles and speeds of a missile’s meeting with an obstacle to trigger blasting device

Authors
Keywords:
Array, Array, Array
Abstract

The article proposes a methodical approach and presents the results of a numerical experiment to calculate and confirm the specified parameters of the functioning of the safety-actuating mechanism for reliable undermining of the warhead under various conditions of encountering an unmanaged aircraft rocket with the surface. In order to confirm the results of the calculation methodology, the article discusses the method of real-time reproduction of the actuation of the safety mechanism, as well as a schematic diagram and a description of the operation of such a test device.

Author Biographies
  1. A. L. Zirka, Central Scientific Research Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Candidate of Technical Sciences

  2. V, S, Silkov, Central Scientific Research Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Candidate of Technical Sciences
    docent

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

    Candidate of Technical Sciences
    Senior Research Fellow

References
Cover Image
Published
2019-09-26
Section
AIRCRAFT ARMAMENT & FACILITIES
License
Creative Commons License

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

How to Cite

Method of calculating of the range of angles and speeds of a missile’s meeting with an obstacle to trigger blasting device. (2019). Weapons and Military Equipment, 23(3), 78-83. https://doi.org/10.34169/2414-0651.2019.3(23).78-83

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