| 期 |
栏目 |
标题 |
文件 |
| 卷 15, 编号 1 (2014) |
Articles |
Influence of design parameters of a flow regulator on its static and dynamic characteristics |
(Rus)
|
| 卷 13, 编号 5 (2012) |
Articles |
EXPERIMENTAL INVESTIGATIONS OF INCOMPRESSIBLE VISCOUS FLUID IN THE FRONT GAP BETWEEN ROTATING DISK AND FIXED BOUNDARY |
(Rus)
|
| 卷 24, 编号 2 (2023) |
Section 3. Technological Processes and Materials |
Simulation model of the system for ensuring the intraclimatic characteristics of clean industrial premises of space industry enterprises |
(Rus)
|
| 卷 23, 编号 4 (2022) |
Section 2. Aviation and Space Technology |
Methodology for assessing reliability of stand-bed systems in testing liquid throat engines |
(Rus)
|
| 卷 23, 编号 1 (2022) |
Section 2. Aviation and Space Technology |
Analysis of the stress-deformed state of the prismatic support of the lever-grading device of test stands for liquid rocket engines |
(Rus)
|
| 卷 23, 编号 3 (2022) |
Section 2. Aviation and Space Technology |
Method for processing the results of cavitation tests of TNA pumps in order to obtain an approximating function |
(Rus)
|
| 卷 23, 编号 3 (2022) |
Section 2. Aviation and Space Technology |
Modeling and verification of working process parameters in gas generators for pressurizing fuel tanks of liquid propellant rocket propulsion systems |
(Rus)
|
| 卷 22, 编号 3 (2021) |
Section 2. Aviation and Space Technology |
Flow model in the impeller of a centrifugal pump |
(Rus)
(Eng)
|
| 卷 22, 编号 2 (2021) |
Section 2. Aviation and Space Technology |
Characteristics of low thrust liquid-propellant rocket engines testing process |
(Rus)
(Eng)
|
| 卷 22, 编号 4 (2021) |
Section 2. Aviation and Space Technology |
Comparative analysis of verified numerical simulation of cavitation based on the Rayleigh – Plesset model for liquid propellant rocket engine pumps |
(Rus)
(Eng)
|
| 卷 21, 编号 3 (2020) |
Section 2. Aviation and Space Technology |
CFD methods for cavitation modeling in centrifugal and axial pumps of LRE |
(Eng)
|
| 卷 20, 编号 2 (2019) |
Section 2. Aviation and Space Technology |
The method of the disk friction determining of low mass flow centrifugal pumps |
(Eng)
|
| 卷 20, 编号 2 (2019) |
Section 3. Technological Processes and Materials |
The process of nanomodifying cast aluminum alloy ingots for components of aerospace vehicles |
(Eng)
|
| 卷 21, 编号 2 (2020) |
Section 2. Aviation and Space Technology |
The method of the disk friction determining of low mass flow centrifugal pumps |
(Eng)
|
| 卷 21, 编号 2 (2020) |
Section 3. Technological Processes and Materials |
The process of nanomodifying cast aluminum alloy ingots for components of aerospace vehicles |
(Eng)
|
| 卷 24, 编号 4 (2023) |
Section 2. Aviation and Space Technology |
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology |
(Rus)
(Eng)
|
| 卷 25, 编号 3 (2024) |
On the occasion of centenary of the birth of academician M. F. Reshetnev |
Innovative technical solutions developed under the leadership of M. F. Reshetnev in the creation of the first Siberian launcher “Cosmos-3M” |
(Rus)
(Eng)
|
| 卷 25, 编号 3 (2024) |
Section 2. Aviation and Space Technology |
Implementation of additive 3D printing technology in the development of an experimental oxygen-hydrogen low thrust rocket engine |
(Rus)
(Eng)
|
