Email this article Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
- Authors: Konstantinov S.V.1,2, Lalabekov V.I.2, Obolenskii Y.G.2,3
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Affiliations:
- Branch PAO “Kompaniya Sukhoi”
- Moscow Aviation Institute
- Russian Aircraft Corporation “MiG”
- Issue: Vol 62, No 2 (2019)
- Pages: 222-228
- Section: 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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Abstract
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.
About the authors
S. V. Konstantinov
Branch PAO “Kompaniya Sukhoi”; Moscow Aviation Institute
Email: lalabekov.valentin@yandex.ru
Russian Federation, ul. Polikarpova 23a, Moscow, 125284; Volokolamskoe sh. 4, Moscow, 125993
V. I. Lalabekov
Moscow Aviation Institute
Author for correspondence.
Email: lalabekov.valentin@yandex.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
Yu. G. Obolenskii
Moscow Aviation Institute; Russian Aircraft Corporation “MiG”
Email: lalabekov.valentin@yandex.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993; 1-i Botkinskii proezd 7, Moscow, 125284
