Substantiation of design and technological parameters of anti-meteoroid protection for critical elements of modern spacecraft
Authors: Smirnov A.V., Mikhailova M.A. | Published: 13.12.2021 |
Published in issue: #12(65)/2021 | |
DOI: DOI: 10.18698/2541-8009-2021-12-753 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: space debris, spacecraft, impact interaction, shield, high velocity impact, ballistic curve, numerical simulation, protective structures |
Analysis of the influence of the matrix geometry on the thinning of the domed part of sheet metal parts during lead stamping
Authors: Ivanov D.A. | Published: 25.11.2020 |
Published in issue: #10(51)/2020 | |
DOI: DOI: 10.18698/2541-8009-2020-10-646 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: stamping with plastic metal, thin-walled part, lead-in part of the matrix, thinning of the dome part, design modeling, DEFORM-2D software package, setting the calculation parameters |
The methodology for analyzing the base of diagrams of the stress-strain state of materials in the software-mathematical environment Deform-3D to study the processes of plastic deformation
Authors: Boyarskiy D.S. | Published: 04.03.2020 |
Published in issue: #2(43)/2020 | |
DOI: DOI: 10.18698/2541-8009-2020-2-581 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: stress-strain state of the material, diagrams of true and conditional stress, corrosion-resistant steel, titanium and aluminum alloys, models of the deformable body, mathematical relationships between stresses and strains, compression and tension of cylindrical samples, finite element model, Deform-3D program |
Forecasting launches of certain types of satellites for the long term using the extrapolation method
Authors: Pivovarov V.A., Soboleva T.N., Tsigankova E.A. | Published: 27.03.2019 |
Published in issue: #3(32)/2019 | |
DOI: DOI: 10.18698/2541-8009-2019-3-454 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: satellite, forecasting, analysis, space market, launches, space junk, trend model, spacecraft |
Analysis of debris of the near-earth space and objects of man-made pollution
Authors: Pivovarov V.A., Soboleva T.N., Tsigankova E.A. | Published: 20.12.2018 |
Published in issue: #12(29)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-12-418 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: space debris, satellite, spacecraft, clogging, orbit, collision, trend, near-earth space, debris |
Concept of spacecraft with electric jet engine on outboard air
Authors: Kulnov A.S. | Published: 06.11.2018 |
Published in issue: #10(27)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-10-395 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: hall-effect engine, accelerating voltage, thrust power, air resistance, air intake, electrical capacity, low earth orbit, spacecraft |
Calculating and optimizing the mass-dimensional parameters of the radiator in the closed space-based gas turbine plants
Authors: Komarov E.M. | Published: 24.09.2018 |
Published in issue: #9(26)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-9-376 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: radiator, spacecraft, construction, analysis, closed gas turbine plant, heat exchange, electric-power installation, finning |
Implementation of the universal asynchronous receiver-transmitter on the programmable logical integrated circuit die
Authors: Ronzhin I.V., Makarova A.V. | Published: 12.04.2018 |
Published in issue: #4(21)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-4-295 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: programmable logical integrated circuits, universal asynchronous receiver-transmitter, UART data protocol, RX receiver circuit, TX transmitter circuit, implementation of UART in programmable logical integrated circuits |
Comparative analysis of the operation of liquid-fuel rocket engine pump turbine if equipped with the auxiliary booster pump package
Authors: Ivashin V.S., Anishchenko Yu.V. | Published: 20.12.2017 |
Published in issue: #1(18)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-1-225 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: pump turbine, booster pump package, fuel feed system, spin rate, pump speed coefficient, rocket engine |
Developing the parameters determination program for defining the trajectory of the sub-orbital re-entry space vehicle of the tourist class
Authors: Kapitonov D.D. | Published: 09.10.2017 |
Published in issue: #10(15)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-10-186 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: re-entry space vehicle, flight trajectory, pitch angle, angle of attack, flight altitude |