Principles of Designing and Ensuring Reliability of Parachute Systems for Foreign Manned Spacecraft
Authors: Ploskov S.Yu. | Published: 12.09.2022 |
Published in issue: #3(142)/2022 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: parachute system, reliability, parachute clusters, descent spacecrafts, redundancy, designing, parachute system operation |
Roller Profiling for Shaping Corrugated Profiles on the Heat Exchanger Tape for Wind Tunnels
Authors: Shchipkova Yu.V., Popov A.Yu. | Published: 25.06.2021 |
Published in issue: #2(137)/2021 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: profiling, roller, rolling, corrugated tape, centroid, tooth profile, tool, springing |
Investigating Curing Kinetics for a Thin-Walled Carbon Fibre Structure
Authors: Chen Ya., Maung P.P., Malysheva G.V. | Published: 19.10.2020 |
Published in issue: #5(134)/2020 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: carbon fibre, vessel, simulation, kinetics, temperature gradient, curing |
Developing a Movable Part for a Test Bench Featuring a Linear Motor and Magnetic Suspensionfor Simulating Inertial Loads on an Object
Authors: Lobastov I.A., Paleshkin A.V. | Published: 18.10.2020 |
Published in issue: #5(134)/2020 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: space capsules, development testing, centrifugal test bench, linear motor, magnetic suspension, aerospace engineering, high-temperature superconducting elements |
Investigation of the Ballistic Descent Mode for a Maneuverable Lander to the Venus Surface
Authors: Kosenkova A.V., Minenko V.E., Agafonov D.N. | Published: 11.08.2020 |
Published in issue: #4(133)/2020 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: landing module, lifting body, descent trajectory, Venus, lateral manoeuvre |
Non-Linear Model Dynamics Analysis for Aerospace Engineering Structures Subjected to Non-Steady-State Random Loads
Authors: Tushev O.N., Belyaev A.V., Wang Yizhou | Published: 17.02.2020 |
Published in issue: #1(130)/2020 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: forced oscillation equations, stochastic analysis, external (additive) and parametric (multiplicative) effects, statistical linearisation, fundamental matrix, multiplicative integral, integropower series |
On Computing the Stress-Strain State of a Transformable Large-Scale Space Structure
Authors: Zhang Z., Zimin V.N. , Krylov A.V., Churilin S.A. | Published: 16.02.2020 |
Published in issue: #1(130)/2020 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: transformable structure, load-bearing framework, stress-strain state, deployment |
Investigation of the Influence of Structural and Adjusting Parameters of a Quadruple-Orifices Electrohydraulic Amplifier on the Static Characteristics of Rocket Pack Steering Actuator
Authors: Belonogov O.B. | Published: 20.12.2019 |
Published in issue: #6(129)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: structural and adjusting parameters, electrohydraulic amplifier, steering actuator, static characteristics |
Technique Employing Topology Optimisation to Determine Panel-to-Panel Support Bracket Positions in a Spacecraft Body
Authors: Borovikov A.A., Leonov A.G., Tushev O.N. | Published: 03.09.2019 |
Published in issue: #4(127)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: topology optimisation, finite element method, dynamic compatibility, spacecraft, technique |
Mathematical Simulation of Using a Combination of Mesh and Porous Materials as a Phase Separator
Authors: Avraamov N.I., Korolkov A.V., Maslov V.A., Sapozhnikov V.B. | Published: 19.07.2019 |
Published in issue: #3(126)/2019 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: mathematical simulation, combination of mesh and porous materials, bulk capillary properties, phase separator, in-tank inlet devices, critical retention capacity, residual propellant |