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Attitude and Orientation Control System [AOCS]

Kinetic Moment Reset System 1207

  • Purpose: Calming the low-orbit spacecraft and dumping the accumulated kinetic moment from the spacecraft body and flywheel engines.
  • Year of release: 2014
  • Guaranteed service life (years): 10
  • Estimated production / delivery time (months): 14
  • Flight qualification of the product: Да
  • Brief history of flight qualification: As part of the spacecraft "Meteor-M".
  • Possibility to adapt the product to customer requirements: Да
ParameterValue
Working orbitsLow, medium
Weight35 kg
Maximum power consumption50 W
The working magnetic moment of each electromagnet400 Am2

Kinetic moment reset system. Structurally, the product consists of: - 2 primary converters of the geomagnetic field PGP-3M, PGP-3MD (duplicate); - 3 electromagnets (length - 0.85 m), forming three axis rod electromagnets; - electronic block.