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 | |
Analysis of spacecraft launches to the planets of the solar system
| Authors: Konoplyanova I.A., Kireev I.M. | Published: 23.12.2020 |
| Published in issue: #12(53)/2020 | |
| DOI: DOI: 10.18698/2541-8009-2020-12-663 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
| Keywords: analysis, launch, spacecraft, trend model, planet, solar system, forecast, forecasting methods | |
Literature review of methods for obtaining holes in composite materials
| Authors: Khokhlov Yu.N., Klyushnikov M.V., Prokhorova M.A. | Published: 24.12.2020 |
| Published in issue: #1(54)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-1-664 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
| Keywords: hole forming, piercing method, polymer composite material, laser cutting, ultrasonic processing, ultrajet technology, mechanical shaping | |
Investigation of the movement of the descent vehicle in the planet’s atmosphere taking into account the asymmetry
| Authors: Kukharenko A.S. | Published: 27.04.2021 |
| Published in issue: #4(57)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-4-691 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: descent vehicle, differential equations, stable motion, oscillations, coordinate system, damping moment, angle of attack, rotational motion | |
Creation of a defective CFRP panel for testing methods of its control and cutting
| Authors: Tsypysheva S.N., Ternovskikh K.A., TSzia CHzheniuan | Published: 17.06.2021 |
| Published in issue: #5(58)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-5-703 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
| Keywords: composite part defects, adhesion, delamination, contact molding, carbon prepreg, acoustic emission, non-destructive testing | |
Anomalies of the Earth’s gravitational field in applied problems of ballistics
| Authors: Kolesnikova D.S. | Published: 08.07.2021 |
| Published in issue: #6(59)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-6-709 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: full vector of the gravitational field strength, anomalous gravitational field, Earth ellipsoid, Krasovsky ellipsoid, central gravitational field, model of the Earth’s figure, mathematical modeling, trajectory of an aircraft | |
Features of hypersonic aircraft use
| Authors: Vafina E.A. | Published: 08.07.2021 |
| Published in issue: #6(59)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-6-710 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: hypersonic aircraft, control, controllability, control methods, maneuvering, missile technology, weapons, control process, control efficiency | |
Features of the use of Earth’s gravity models in applied problems of ballistics
| Authors: Kolesnikova D.S. | Published: 23.09.2021 |
| Published in issue: #9(62)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-9-737 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: total vector of gravitational field strength, anomalous gravitational field, general terrestrial ellipsoid, Krasovsky ellipsoid, Cleraud ellipsoid, model of the Earth’s figure, mathematical modeling, trajectory of an aircraft | |
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 | |
The choice of an anti-adhesive composition for working with samples from a polymer composite material
| Authors: Dynchenkova T.V., Orlov A.D., Popov Vs.V., Yanko M.A. | Published: 15.12.2021 |
| Published in issue: #12(65)/2021 | |
| DOI: DOI: 10.18698/2541-8009-2021-12-756 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
| Keywords: composite materials, release agent, contact surface treatment, surface quality, product integrity, auxiliary materials, glass fabric | |