FIELD: transport.
SUBSTANCE: invention relates to space hardware testing, namely to installations for simulation of spacecraft components operation modes. Installation for vacuum thermocycling of photoconverter panels includes vacuum chamber consisting of two communicating compartments. In one compartment, two cryopanels are installed in parallel with possibility to place tested panel between them. In the second compartment there is thermal panel made as assembly of filament lamps. The cryopanels and thermal panel are positioned vertically, and thermal panel compartment is placed over cryopanel compartment. The cryopanels are installed with possibility of additional placement of thermal panel between them. The thermal panel is provided with reciprocating mechanism of vertical action and thermal insulation at the side facing cryopanel.
EFFECT: higher accuracy of thermal simulation of outer space conditions.
3 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| INSTALLATION FOR THERMOCOUPLE TESTS OF PANELS OF PHOTOCONVERTERS | 2020 |
|
RU2739231C1 |
| HEAT-ABSORBING PANEL FOR VACUUM THERMAL CYCLING | 2011 |
|
RU2458433C1 |
| DEVICE FOR THERMAL CYCLE TESTING OF PANELS OF PHOTOELECTRIC BATTERIES | 1992 |
|
RU2040076C1 |
| INSTALLATION FOR TESTING THE THERMAL STABILITY OF SAMPLES OF PHOTOVOLTAIC BATTERIES | 2022 |
|
RU2787936C1 |
| SOLAR BATTERY FOR SMALL-SIZE SPACECRAFTS AND METHOD OF ITS MANUFACTURING | 2013 |
|
RU2525633C1 |
| METHOD OF THERMAL-VACUUM TESTS OF SPACE VEHICLES AND DEVICE FOR ITS IMPLEMENTATION | 2014 |
|
RU2565149C2 |
| METHOD OF TREATING STEEL OBJECTS | 1995 |
|
RU2094484C1 |
| THERMAL INSULATION UNIT | 0 |
|
SU1826043A1 |
| SOLAR BATTERY | 1999 |
|
RU2156522C1 |
| PULSE AIR WIND TUNNEL | 0 |
|
SU1577487A1 |
