Шығарылым |
Бөлім |
Атауы |
Файл |
Том 13, № 1 (2012) |
Articles |
FEATURES OF EXPERIMENTAL DEFINITION OF COMPOSITE MATERIALS DURABILITY AGAINST EROSIVE IMPACT OF STATIONARY PLASMA THRUSTERS |
 (Rus)
|
Том 24, № 1 (2023) |
Section 2. Aviation and Space Technology |
The main provisions of the methodology for ensuring the resistance of the onboard equipment of spacecraft to the effects of the radiation effects of outer space |
 (Rus)
|
Том 11, № 1 (2010) |
Articles |
Indicatrix account of materials dispersion at the estimations of erosion-contaminating influence of streams of plasma thrusters on space craft |
 (Rus)
|
Том 24, № 1 (2023) |
Section 2. Aviation and Space Technology |
Possibility of unification of requirements for radiation resistance for spacecraft with different operating conditions |
 (Rus)
|
Том 24, № 2 (2023) |
Section 2. Aviation and Space Technology |
Problematic issues of application of methods of accelerated radiation testing of ECB |
 (Rus)
|
Том 23, № 2 (2022) |
Section 2. Aviation and Space Technology |
Pressure measurement inside non-sealed equipment bay of the geostationary spacecraft |
 (Rus)
|
Том 21, № 4 (2020) |
Section 2. Aviation and Space Technology |
Influence of plasma jets of electric jet engines on spacecraft functional characteristics |
 (Eng)
|
Том 25, № 2 (2024) |
Section 2. Aviation and Space Technology |
Results of monitoring the radiation environment in medium circular orbit |
 (Rus)
 (Eng)
|
Том 25, № 1 (2024) |
Section 2. Aviation and Space Technology |
Issues of ensuring the resistance of high-voltage solar arrays of spacecraft to the effects of secondary arc discharges |
 (Rus)
 (Eng)
|
Том 26, № 2 (2025) |
Section 2. Aviation and Space Technology |
Radiation conditions in medium circular orbit during the extreme magnetic storm in May 2024 |
 (Rus)
 (Eng)
|