电邮这篇文章 Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
- 作者: Konstantinov S.1,2, Lalabekov V.2, Obolenskii Y.2,3
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隶属关系:
- Branch PAO “Kompaniya Sukhoi”
- Moscow Aviation Institute
- Russian Aircraft Corporation “MiG”
- 期: 卷 62, 编号 2 (2019)
- 页面: 222-228
- 栏目: 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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详细
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.
作者简介
S. Konstantinov
Branch PAO “Kompaniya Sukhoi”; Moscow Aviation Institute
Email: lalabekov.valentin@yandex.ru
俄罗斯联邦, ul. Polikarpova 23a, Moscow, 125284; Volokolamskoe sh. 4, Moscow, 125993
V. Lalabekov
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: lalabekov.valentin@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
Yu. Obolenskii
Moscow Aviation Institute; Russian Aircraft Corporation “MiG”
Email: lalabekov.valentin@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993; 1-i Botkinskii proezd 7, Moscow, 125284
