Reflector of the C-band Antenna which Forms Planimetric Directional Diagram
Flight-proven C-band contour reflector (Ø1800 mm, ≤0.5 mm rms surface, 9 kg) on 1830×790 mm boom for planimetric beam antennas.
Technical specifications
- Purpose
- Reflector for C-band antenna forming planimetric directional diagram
- Year of release
- 2012
- Guaranteed service life, years
- 15
- Estimated production/delivery time
- 12 months
- Flight heritage
- In unconditional flight operation since spacecraft launch
- Frequency band
- C
- Reflector aperture diameter, mm
- 1800
- rms deviation of reflecting surface (with utilization factors), mm
- ≤0.5
- Reflector surface type
- Contour
- Boom overall dimensions, mm
- 1830 × 790
- Reflector assembly mass, kg
- 9
- TRL
- 9 (flight-proven)
About
The Reflector of the C-band Antenna which Forms Planimetric Directional Diagram is a flight-qualified C-band reflector assembly for spacecraft antennas forming planimetric directional diagrams. It features a 1800 mm aperture contour reflector with ≤0.5 mm rms surface deviation (accounting for utilization factors), mounted on a 1830 × 790 mm boom. Total reflector assembly mass is 9 kg. Released in 2012 with 15-year service life and 12-month delivery time. In unconditional flight operation since spacecraft launch.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
