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Spacecraft Mechanisms

Reflector Transfer Mechanism

  • Purpose: Antenna deployment and alignment.
  • Year of release: 2013
  • Guaranteed service life (years): 10
  • Estimated production / delivery time (months): 6
ParameterValue
Readjustment/rotation angle for each axis, °±90
Slew rate, °/min0-60
Measurement error of the rotation angle for each axis, arcmin, not exceeding1.5
Developed torque for each axis, N·m, not less than50
Self-braking torque in a de-energized state of the electric motors for each axis, N·m, not less than20
Operating temperature range, °С-40 to +50
Overall dimensions, mm320 х 230 х 230
Mass, kg7
Operational life defined by hours, not less than140000
Active lifetime, years15

Two-degree-of-freedom electromechanical device for transferring the reflector boom from the transportation to the operational position and for antenna reflector pointing after its deployment.