Email this article Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle
- Authors: Sattarov A.G.1, Sochnev A.V.1, Bikmuchev A.R.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- Gagarin Research and Test Cosmonaut Training Center
- Issue: Vol 61, No 2 (2018)
- Pages: 299-303
- Section: Technical Notes Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230543
- DOI: https://doi.org/10.3103/S1068799818020216
- ID: 230543
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Abstract
The location of the center of mass closer to the source of radiation during rectilinear accelerated motion of an aircraft in the absence of gravity and drag forces provides stability of the angular motion. The proposed scheme was analyzed on the basis of the Lagrange–Dirichlet theorem.
About the authors
A. G. Sattarov
Tupolev Kazan National Research Technical University
Email: sochnev.aleksandr@inbox.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
A. V. Sochnev
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: sochnev.aleksandr@inbox.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
A. R. Bikmuchev
Gagarin Research and Test Cosmonaut Training Center
Email: sochnev.aleksandr@inbox.ru
Russian Federation, Zvesdnyi gorodok, Moskovskaya oblast, 141160
