Email this article Structural scheme of a laser-initiated pyrocartridge for use in advanced aerospace systems and its justification by numerical simulation methods
- Authors: Avatinyan G.A.1
-
Affiliations:
- D. I. Mendeleev Russian University of Chemical Technology
- Issue: Vol 15, No 2 (2022)
- Pages: 96-101
- Section: Articles
- URL: https://bakhtiniada.ru/2305-9117/article/view/286750
- DOI: https://doi.org/10.30826/CE22150209
- EDN: https://elibrary.ru/EZBNFQ
- ID: 286750
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Abstract
The paper briefly analyzes the advantages and prospects for the development of laser-initiated pyrotechnics, the existing developments in this area and their current problems. A structural scheme of a laser initiated pyrocartridge, a scheme for focusing light to initiate a pyrotechnic charge, and a method for implementing control of the pressure pulse generated by it are proposed. Numerical simulation methods have been used to study the behavior of the pyrocartridge design under static high-pressure loading and the possibility of generating various pressure pulses in the working volume of spacecraft pyrounits during the outflow of gases from the pyrocartridge after charge initiation.
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About the authors
Grigoriy A. Avatinyan
D. I. Mendeleev Russian University of Chemical Technology
Author for correspondence.
Email: agra89@mail.ru
(b. 1989) – Candidate of Science in technology, research scientist
Russian Federation, 9 Miusskaya Sq., Moscow 125047References
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