Ultra-high vacuum and deep thermal cycling system designed for space components, satellite subsystems, and advanced optical payloads.
Thermal balance and thermal vacuum bake-out of full satellite buses.
Deployment mechanism verification in high-vacuum conditions.
Optical distortion measurement through precision quartz viewports.
Total Mass Loss (TML) and Collected Volatile Condensable Material (CVCM).
| Vacuum Level | High Vacuum (10⁻⁵ to 10⁻⁷ mbar) via Dry Scroll + Turbomolecular / Cryopump |
|---|---|
| Thermal Shroud Temperature | -180°C to +150°C (Liquid Nitrogen LN₂ Cooling + Radiant/Cartridge Heaters) |
| Chamber Geometry | Horizontal Cylindrical or Box-type SS304/SS316L with electropolished finish |
| Feedthrough Flanges | CF / KF / ISO flanges for High-voltage, RF Sub-D, Thermocouple feedthroughs |
| Viewports & Optical Ports | Optically flat fused silica / quartz windows with shutter protection |
| Automated SCADA | Automated thermal cycling profiles, ramp rates, pressure safety interlocks |
Direct consultation with our senior engineering team in Delhi.