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Attitude and Orientation Control System [AOCS]

Kinetic Moment Reset System

  • Purpose: Calming the low-orbit spacecraft and dumping the accumulated kinetic moment from the spacecraft body and flywheel engines.
  • Year of release: 2005
  • Guaranteed service life (years): 10
  • Estimated production / delivery time (months): 14
  • Flight qualification of the product: Yes
  • Brief history of flight qualification: As part of the Resurs-DK spacecraft.
  • Possibility to adapt the product to customer requirements: Yes
ParameterValue
Working orbitsLow, medium
Weight50 kg
Maximum power consumption50 W
The working magnetic moment of each electromagnet1000 Am2

Kinetic moment reset system.

Structurally, the product consists of:

  • 2 primary converters of the geomagnetic field PGP-3M, PGP-3MD (duplicate);
  • 6 electromagnets (each length is 1 m), forming three axis rod electromagnets;
  • electronic block.