Thermal Vacuum Chamber

BST's thermal vacuum chamber allows the qualification and acceptance testing of space systems. Those tests can be performed under high vacuum and well-defined temperature scenarios. Those thermal vacuum tests are fully automated and can easily be run over long periods.

Features thermal:
Vacuum
Solar simulator
Specimen length [mm]: 650.0
Specimen width/dia [mm]: 550.0
Specimen height/thk [mm]: 500.0
Mass max. [kg]: 100.0
Higher temperature [K]: 400.0
Lower temperature [K]: 200.0
Temperature change rate [±K/min]: 2.0
Feedthroughs: 2x 50pin Sub-D / optical viewports (+ optional DN100-CF flange for custom solution)
Data acquisition: temperature sensors, pressure gauge, voltage, current
Vacuum limit [hPa] [mbar]: 1.00E-06
Project heritage: BST Satellite Projects (Kent Ridge 1) and Subsystems (Star Trackers, Reaction Wheels, etc.)
Cleanroom classes (ISO 14644-1):
ISO Class ≤5
ISO Class 6
ISO Class 7
ISO Class 8
ISO Class 9
Keywords/tags: TVAC, Thermal Vacuum, qualification, acceptance, bakeout, cycling, thermal balance

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