Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle
- Авторы: Sattarov A.1, Sochnev A.1, Bikmuchev A.2
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Учреждения:
- Tupolev Kazan National Research Technical University
- Gagarin Research and Test Cosmonaut Training Center
- Выпуск: Том 61, № 2 (2018)
- Страницы: 299-303
- Раздел: 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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Аннотация
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.
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Об авторах
A. Sattarov
Tupolev Kazan National Research Technical University
Email: sochnev.aleksandr@inbox.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
A. Sochnev
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: sochnev.aleksandr@inbox.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
A. Bikmuchev
Gagarin Research and Test Cosmonaut Training Center
Email: sochnev.aleksandr@inbox.ru
Россия, Zvesdnyi gorodok, Moskovskaya oblast, 141160