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Mechanism of formation of the disturbing moment by the mobile mass of a spacecraft
| Authors: Bobkov A.V., Krivenko M.Yu. | Published: 22.04.2026 |
| Published in issue: #5(794)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: spacecraft, internal disturbances, mobile mass, Coriolis moment, kinetic moment |
Software packages for thermal calculation of chemical rocket engines
| Authors: Belov G.V. | Published: 22.05.2026 |
| Published in issue: #6(795)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: thermochemical rocket engine, combustion products, thermodynamic simulation |
The use of hybrid polymer composite materials to regulate the temperature coefficient of linear expansion of forming equipment
| Authors: Iroshnikov A.I., Martirosyan V.S., Polovy A.O., Kovanov A.E. | Published: 02.06.2026 |
| Published in issue: #6(795)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: forming equipment, hybrid PCM, temperature coefficient of linear expansion, reinforcing component, glass-carbon fiber |
Calculation of Displacements to Correct the Mounting Locations of Devices When the Mass Limits Are Exceeded in the Placement Zones in Compartment
| Authors: Belyakov А.А. | Published: 06.07.2026 |
| Published in issue: #7(796)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: center of gravity, moment of inertia, spacecraft, on-board equipment, devices layout, compartment centering |
Methodology for Determining the Optimal Mass Ratio of Fuel Charges for an Aft Gas Generator and a Rocket Engine from the Perspective of Achieving Maximum Range
| Authors: Vetrov V.V., Shilin P.D. | Published: 10.07.2026 |
| Published in issue: #7(796)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: aft gas generator, solid-propellant rocket motor, equivalent specific impulse, base drag, combined propulsion system, maximum flight range |
Modelling of CubeSat satellite motion with inflatable braking device. Part 1. Determination of aerodynamic characteristics and trajectory parameters
| Authors: Guselnikov A.V., Fedyunina E.R., Prosuntsov P.V. | Published: 28.07.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: microsatellite CubeSat, drag force, free-molecular flow, inflatable braking device, direct Monte Carlo simulation method |
Theoretical and experimental study of thermal conductivity and operational limits of a sodium axial heat pipe relative to the gravity vector orientation
| Authors: Borschev N.O., Kochegarova A.V. | Published: 31.07.2026 |
| Published in issue: #8(797)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: axial heat pipe, boiling limit, sonic limit, viscous limit, capillary limit |