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