Method of calculating of the range of angles and speeds of a missile’s meeting with an obstacle to trigger blasting device
DOI:
https://doi.org/10.34169/2414-0651.2019.3(23).78-83Keywords:
unmanaged aircraft rocket, full play, unmanaged air-to-surface rocketAbstract
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.
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References
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4. Silkov, V. I. (1995), “Dinamika poleta letatel’nykh apparatov: konspekt lektsiy” [Flight dynamics of aircraft. Lecture notes], KMUGA, K., 424 р.
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Published
2019-09-26
How to Cite
Zirka, A., Silkov, V., & Zhevtiuk, O. (2019). Method of calculating of the range of angles and speeds of a missile’s meeting with an obstacle to trigger blasting device. Weapons and Military Equipment, 23(3), 78–83. https://doi.org/10.34169/2414-0651.2019.3(23).78-83
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Section
AIRCRAFT ARMAMENT & FACILITIES
