FIELD: testing equipment.
SUBSTANCE: invention is related to the sphere of space engineering. Device for thermal-vacuum tests contains fixed cylindrical cryogenic screen installed in the vacuum chamber, spatially positioned screen with size changing bracket, and drive of 3D dislocation. Method of thermal-vacuum tests is characterized by presence of the remotely moved spatially positioned screen with spatially changed form geometry. The spatially positioned screen ensures variational, differentiated cryostatting of some elements and assemblies of the space vehicle.
EFFECT: increased speed of the test unit setting to the mode, achievement of the lower temperatures for local areas of the tested vehicle.
2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
STAND FOR CONDUCTING THE SPACECRAFT HEAT AND VACUUM TESTS | 2005 |
|
RU2302983C1 |
BENCH FOR CARRYING OUT THERMAL-VACUUM TESTS OF SPACECRAFT UNDER CONDITIONS THAT SIMULATE FULL-SCALE | 2020 |
|
RU2734681C1 |
STAND FOR THERMAL-VACUUM TESTING OF CUBESAT-STANDARD SATELLITES WITH A COMMUNICATION INTERFACE | 2021 |
|
RU2772156C1 |
TEST BENCH FOR SPACECRAFT RADIO ELECTRONIC THERMAL TESTS | 2014 |
|
RU2553411C1 |
METHOD OF HEAT-VACUUM TEST OF SPACECRAFT | 2014 |
|
RU2564056C1 |
STAND FOR THERMAL VACUUM TESTING OF SPACECRAFT ELEMENTS | 2020 |
|
RU2759359C1 |
METHOD FOR OUTGASSING STRUCTURAL ELEMENTS OF SPACECRAFT IN GROUND CONDITIONS | 2021 |
|
RU2778479C1 |
METHOD OF SIMULATION OF EXTERNAL HEAT FLOWS FOR GROUND OPTIMISATION OF SPACECRAFT TEMPERATURE CONTROL | 2012 |
|
RU2519312C2 |
CRYOGENIC VALVE | 2011 |
|
RU2469927C1 |
STAND FOR THERMAL TESTS OF SPACE OBJECTS | 1999 |
|
RU2172709C2 |
Authors
Dates
2015-10-20—Published
2014-01-21—Filed