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Command & Measurement System and Telemetry

Active Weightlessness System

  • Purpose: Ground modal testing under conditions simulating weightlessness and testing of large transformable spacecraft systems deployment, including reflectors with a diameter up to 50 m.
  • Year of release: 2014
  • Guaranteed service life (years): 3
  • Estimated production / delivery time (months): 12
  • Possibility to adapt the product to customer requirements: Yes
ParameterValue
Object suspension error

Active suspension system for large-sized transformable spacecraft systems at ground modal testing. Simultaneously with the suspension, the dynamic parameters are estimated (velocity, acceleration, etc.) with reference to the absolute time scale.