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Attitude and Orientation Control System [AOCS]

Electromagnet EM-IF-20

  • Purpose: Executive electromagnet of stabilization spacecraft equipment.
  • Year of release: 2012
  • Guaranteed service life (years): 12
  • Estimated production / delivery time (months): 8
  • Flight qualification of the product: Да
  • Possibility to adapt the product to customer requirements: Да
ParameterValue
WeightNo more than 0,63 kg
Power consumption2,5 W
Working magnetic momentNot less than 20 Am2
The length of each electromagnet0,35 m

The core electromagnet for the stabilization equipment of the spacecraft with a harness on which the connector is soldered.