FIELD: space technology. SUBSTANCE: method involves simulation of natural heat flows temperatures and pressures, predominantly lower 0.3-1.0 kPa, of gas medium in a thermal vacuum chamber. The tests are performed in dry air. EFFECT: improved accuracy. 1 tbl
Title | Year | Author | Number |
---|---|---|---|
METHOD OF FREEZING THERMAL VACUUM CHAMBER AND THERMAL VACUUM CHAMBER | 0 |
|
SU1805223A1 |
METHOD OF TESTING OBJECTS IN THERMAL PRESSURE CHAMBER | 0 |
|
SU1742600A1 |
PERAMBULATOR COMBINATION RUNNING GEAR | 1991 |
|
RU2025366C1 |
METHOD OF HEAT-VACUUM TEST OF SPACECRAFT | 2014 |
|
RU2564056C1 |
GROUND EXPERIMENTAL COMPLEX SIMULATING PROLONGED SPACE FLIGHTS, MARS-MISSION INCLUDED | 2007 |
|
RU2329184C1 |
ADSORPTION HIGH-VACUUM PUMP | 0 |
|
SU1753032A1 |
VACUUM INSTALLATION FOR THERMAL TESTS | 0 |
|
SU1455044A1 |
VACUUM INSTALLATION FOR THERMAL TESTING | 0 |
|
SU1599577A2 |
"PYROGARMONY" MUSICAL INSTRUMENT | 2019 |
|
RU2717918C1 |
METHOD OF INFRARED EVALUATION OF COSMONAUTE ADAPTATION TO LONG INTERPLANETARY PILOT FLOWS | 2016 |
|
RU2621305C1 |
Authors
Dates
1994-03-15—Published
1992-04-14—Filed