Отправить статью по E-mail Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
- Авторы: Konstantinov S.1,2, Lalabekov V.2, Obolenskii Y.2,3
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Учреждения:
- Branch PAO “Kompaniya Sukhoi”
- Moscow Aviation Institute
- Russian Aircraft Corporation “MiG”
- Выпуск: Том 62, № 2 (2019)
- Страницы: 222-228
- Раздел: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230926
- DOI: https://doi.org/10.3103/S1068799819020077
- ID: 230926
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Аннотация
The mathematical model and research results of processes running in the interconnected system of “solid propellant propulsion system—swiveling controlled nozzle—flexible joint—gas-hydraulic actuator” are represented. The possibility of increasing the aircraft efficiency due to the inherent features of the system under study is shown.
Об авторах
S. Konstantinov
Branch PAO “Kompaniya Sukhoi”; Moscow Aviation Institute
Email: lalabekov.valentin@yandex.ru
Россия, ul. Polikarpova 23a, Moscow, 125284; Volokolamskoe sh. 4, Moscow, 125993
V. Lalabekov
Moscow Aviation Institute
Автор, ответственный за переписку.
Email: lalabekov.valentin@yandex.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
Yu. Obolenskii
Moscow Aviation Institute; Russian Aircraft Corporation “MiG”
Email: lalabekov.valentin@yandex.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993; 1-i Botkinskii proezd 7, Moscow, 125284
