| Radar | Radiometer | ||
| Polarization | VV, HH and HV | V, H and U | |
| Resolution | 3 km | 10 km | 40 km |
| Relative Error | 1.0 dB | 0.45 dB | 0.64 K |

Hydros instrument makes a conical scan at constant incidence angle over a wide swath.
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The radar and radiometer systems
will share a lightweight, deployable mesh reflector. A
feedhorn will be used with the shared aperture to form an
offset beam with a surface incidence angle of 39.3
deg.
The antenna system will operate
at 1.26 GHz for the radar and 1.41 GHz for the radiometer
and will be capable of both horizontal and vertical
polarizations. The reflector will rotate about the nadir
axis at 14.6 rpm to provide contiguous coverage over the
1000-km swath.
A 6-m reflector will be required
to produce the radiometer footprint of approximately 40
km (root ellipsoidal area), where the resolution is
defined by the antenna 1-way 3-dB beamwidth. Similarly,
the radar 2-way 3-dB real aperture footprint will be 30
km.
The antenna reflector will most likely employ either a folding radial rib or
perimeter truss wire-mesh design. Both are high heritage space-proven designs
which will result in a reflector surface that meets or exceeds the performance
requirements at the desired L-band frequency. A selection decision of the
final reflector design will be made early in the Hydros mission formulation
phase.
To obtain the required 3-km x
3-km and 10-km x 10-km resolution geophysical products,
the radar will employ range and Doppler discrimination.
While similar to standard synthetic aperture radar (SAR),
the aperture length of Hydros will be quite short (32
ms), simplifying the processing. Due to squint angle
effects, the high-resolution products will not be
achieved within a 300-km swath region centered on the
nadir track. Due to the slowly precessing orbit, those
regions will be imaged at the full resolution on later
passes.
