C-band Antenna which Forms Planimetric Directional Diagram
- Purpose: Forming required servicing area; signal reception within the operating frequency band.
- Year of release: 2012
- Guaranteed service life (years): 15
- Estimated production / delivery time (months): 15
- Brief history of flight qualification: Antenna goes through flight operation unconditionally since the launch of the spacecraft.
Parameter | Value |
---|---|
Frequency band | С |
Aperture diameter of reflectors | 1000 and 1600 mm |
rms deviation of the reflectors reflecting surface profile taking into account utilization factors | not exceeding 0.5 mm |
Reflector reflecting surface | contour |
Mass of a reflector with the aperture 1000 mm assembly | 4.7 kg |
Mass of a reflector with the aperture 1600 mm assembly | 8.4 kg |
Spacecraft antenna.
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