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Command & Measurement System and Telemetry

Automatic Control System of Thermal-vacuum-testing

  • Purpose: Automatic control of thermal vacuum testing course of spacecraft in a vacuum chamber. Off-nominal situations analysis.
  • Year of release: 2011
  • Guaranteed service life (years): 5
  • Estimated production / delivery time (months): 12
  • Possibility to adapt the product to customer requirements: Yes
ParameterValue
Vacuum chamber temperature range±150 C
Duration of continuous tests without failing>720 hours
Volume of the horizontal vacuum chamber, m3600
Number of product test pointsmore than 750
Number of controlled parametersmore than 2000

Automatic control system of thermal-vacuum-testing for spacecraft.