Мақаланы E-mail арқылы жіберу Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
- Авторлар: Konstantinov S.V.1,2, Lalabekov V.I.2, Obolenskii Y.G.2,3
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Мекемелер:
- Branch PAO “Kompaniya Sukhoi”
- Moscow Aviation Institute
- Russian Aircraft Corporation “MiG”
- Шығарылым: Том 62, № 2 (2019)
- Беттер: 222-228
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
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.
Авторлар туралы
S. Konstantinov
Branch PAO “Kompaniya Sukhoi”; Moscow Aviation Institute
Email: lalabekov.valentin@yandex.ru
Ресей, ul. Polikarpova 23a, Moscow, 125284; Volokolamskoe sh. 4, Moscow, 125993
V. Lalabekov
Moscow Aviation Institute
Хат алмасуға жауапты Автор.
Email: lalabekov.valentin@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
Yu. Obolenskii
Moscow Aviation Institute; Russian Aircraft Corporation “MiG”
Email: lalabekov.valentin@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993; 1-i Botkinskii proezd 7, Moscow, 125284
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