Chapter: Aviation and Rocket-Space Engineering | Engineering Journal: Science and Innovation

Aspects of applying combined mass–time functional in solving the problem of optimizing the multiple-burn transfer of a spacecraft into a high-energy orbit

Published: 21.03.2022

Authors: Kiriliuk E.V., Stepanov M.N.

Published in issue: #3(123)/2022

DOI: 10.18698/2308-6033-2022-3-2164

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Planning process to ensure the intended use of the optical telescopes system on board the Russian segment of the International Space Station: implementation features

Published: 21.03.2022

Authors: Toporkov A.G., Belyaev A.M.

Published in issue: #3(123)/2022

DOI: 10.18698/2308-6033-2022-3-2165

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

On the issue of optimizing the supersonic business aircraft layout in order to reduce sonic boom

Published: 25.04.2022

Authors: Tyushina M.A., Tyushin A.V., Safin R.M.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2170

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

A thermal mathematical lumped-parameter model of AIST small spacecraft: verification by experimental telemetry data

Published: 25.04.2022

Authors: Kaurov I.V.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2171

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

A thermal mathematical lumped-parameter model of AIST small spacecraft: verification by experimental telemetry data

Published: 25.04.2022

Authors: Kaurov I.V.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2171

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

Modern trends in the development of membrane technologies and their application in launch complex thermostatic control systems

Published: 25.04.2022

Authors: Barmin I.V., Kozlov V.V., Krylov P.V., Mikhaylova I.P.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2172

Category: Aviation and Rocket-Space Engineering | Chapter: Ground Complexes, Launch Equipment, Aircraft Exploitation

Development of direct systems for emergency evacuation from high-altitude units of launch complexes for integrated launch vehicles: exploratory study

Published: 25.04.2022

Authors: Igritsky V.A.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2173

Category: Aviation and Rocket-Space Engineering | Chapter: Ground Complexes, Launch Equipment, Aircraft Exploitation

Deflection of structural elements in estimating parameters of the controlled motion of the descent vehicle with an inflatable braking device

Published: 25.04.2022

Authors: Koryanov V.V., Kukharenko A.S.

Published in issue: #4(124)/2022

DOI: 10.18698/2308-6033-2022-4-2174

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

An approach to choosing the configuration of a supersonic passenger aircraft air intake

Published: 19.05.2022

Authors: Nikolaeva A.A., Serebryanskiy S.A.

Published in issue: #5(125)/2022

DOI: 10.18698/2308-6033-2022-5-2176

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

Application of honeycomb panel structures in spacecraft

Published: 19.05.2022

Authors: Ivanov E.A., Ikonnikova A.A., Kleshnina I.A., Nagovitsin V.N., Pokhabov A.Yu.

Published in issue: #5(125)/2022

DOI: 10.18698/2308-6033-2022-5-2177

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

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