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Formation of schematic solutions for separation systems of ultrasmall-lift launch vehicles based on architectural modeling and classification of their schematic features
| Authors: Kabanov А.А., Borisov V.D. | Published: 11.10.2026 |
| Published in issue: #11(800)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: ultrasmall-lift launch vehicles, mechanical separation systems, Arcadia method, schematic features, Capella, classification of separation systems |
An integrated approach to creating a geometric model of a turbojet engine combustion chamber via reverse engineering
| Authors: Matveev Yu.V., Balakin A.M., Kanakin M.K., Laptev M.A., Barskov V.V., Nurkov I.R. | Published: 05.10.2026 |
| Published in issue: #10(799)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: reverse engineering, 3D scanning, combustion chamber, turbojet engine, CAD |
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 |
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 |
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 |
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 |
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 |
Comparative assessment of tribotechnical characteristics of hard-lubricating coatings of various application methods and friction conditions in relation to tests in a normal atmosphere and in a vacuum
| Authors: Khopin P.N., Mishakov S.Yu. | Published: 10.02.2026 |
| Published in issue: #2(791)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: solid lubricating coatings, tribotechnical characteristics, conditions of a normal atmosphere, various methods of application |
Analysis of a hermetic cabin of a passenger aircraft as a temperature controlled object
| Authors: Grishina L.A., Panevin A.Yu. | Published: 29.01.2026 |
| Published in issue: #2(791)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: aviation environmental control system, the hermetic cabin of the aircraft, thermal control subsystem, transfer function of the hermetic cabin, air temperature |
Experimental studies of the ion plasma thruster for very low orbit spacecraft
| Authors: Fedyanin V.V., Shalai V.V. | Published: 20.01.2026 |
| Published in issue: #1(790)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: very low orbit, ion thruster, ion plasma thruster, radio frequency helicon plasma thruster, Hall-effect thruster, propulsion system |