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Spacecraft Mechanisms

Mechanical Unit of Antenna Pointing System. Type 3

  • Purpose: Provides rotation of the mounting plane for antenna relative to the mounting plane of the antenna pointing system control module in two mutually perpendicular planes.
  • Estimated production / delivery time (months): 6
ParameterValue
Rotation angle for each axis, °± 10; ± 90
Slew rate, °/min0.009- 7.2
Measurement error of the rotation angle for each axis, arcsec, not exceeding90
Developed torque for each axis, N·m, not less than60
Load inertia moment, kg·m2, not exceeding160
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
Operational life defined by hours, not less than10000
Active lifetime, years15
Overall guaranteed lifetime, years19

Two-degree-of-freedom electromechanical drive for antenna pointing.