Enviar artigo por via de e-mail Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
- Autores: Konstantinov S.V.1,2, Lalabekov V.I.2, Obolenskii Y.G.2,3
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Afiliações:
- Branch PAO “Kompaniya Sukhoi”
- Moscow Aviation Institute
- Russian Aircraft Corporation “MiG”
- Edição: Volume 62, Nº 2 (2019)
- Páginas: 222-228
- Seção: 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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Resumo
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.
Sobre autores
S. Konstantinov
Branch PAO “Kompaniya Sukhoi”; Moscow Aviation Institute
Email: lalabekov.valentin@yandex.ru
Rússia, ul. Polikarpova 23a, Moscow, 125284; Volokolamskoe sh. 4, Moscow, 125993
V. Lalabekov
Moscow Aviation Institute
Autor responsável pela correspondência
Email: lalabekov.valentin@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
Yu. Obolenskii
Moscow Aviation Institute; Russian Aircraft Corporation “MiG”
Email: lalabekov.valentin@yandex.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993; 1-i Botkinskii proezd 7, Moscow, 125284
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