| Issue |
Section |
Title |
File |
| Vol 14, No 4 (2013) |
Articles |
THE DESIGN OF THE EXPERIMENT AND CREATION OF THE REGRESSION MODEL OF THE SPECIFIC IMPULSE LIQUID ROCKET ENGINE THRUST FROM 10 TO 420 N |
(Rus)
|
| Vol 15, No 1 (2014) |
Articles |
Influence of design parameters of a flow regulator on its static and dynamic characteristics |
(Rus)
|
| Vol 13, No 2 (2012) |
Articles |
MATHEMATICAL MODELING OF GAS-LIQUID FLOW IN MICROCHANNELS OF VARIOUS GEOMETRY UNDER CHEMICAL REACTIONS, FRICTION AND HEAT EXCHANGE |
(Rus)
|
| Vol 23, No 4 (2022) |
Section 2. Aviation and Space Technology |
Methodology for assessing reliability of stand-bed systems in testing liquid throat engines |
(Rus)
|
| Vol 22, No 1 (2021) |
Section 2. Aviation and Space Technology |
Development of the concept of a reusable liquid rocket engine with three-component fuel |
(Rus)
(Eng)
|
| Vol 22, No 2 (2021) |
Section 2. Aviation and Space Technology |
Design of the cooling system of a reasuble liquid rocket engine with three-component fuel |
(Rus)
(Eng)
|
| Vol 20, No 2 (2019) |
Section 2. Aviation and Space Technology |
Solar thermal propulsion systems with various high-temperature power sources |
(Eng)
|
| Vol 21, No 2 (2020) |
Section 2. Aviation and Space Technology |
Solar thermal propulsion systems with various high-temperature power sources |
(Eng)
|
| Vol 26, No 3 (2025) |
Section 2. Aviation and Space Technology |
Flight efficiency of solar thermal propulsion with double-stage thermal energy storage |
(Rus)
(Eng)
|
