Cryosat-2’s primary payload will be the SAR/Interferometric Radar Altimeter (SIRAL), which has extended capabilities to meet the measurement requirements for ice-sheet elevation and sea-ice freeboard. Cryosat-2 will also carry three star trackers for measuring the orientation of the baseline. In addition, a radio receiver called Doppler Orbit and Radio Positioning Integration by Satellite (DORIS) and a small laser retroreflector will ensure that Cryosat-2’s position is accurately tracked.
SIRAL is an altimeter/interferometer operating in Ku-band (13.575 GHz) in three modes:
– Low-resolution, nadir-pointing altimeter mode
The altimeter will measure the distance between the satellite and the surface of the Earth.
– SAR mode
Unlike conventional radar altimeters, where the interval between pulses is about 500 microseconds, the Cryosat altimeter will send a burst of pulses with an interval of only 50 microseconds between them. The returning echoes will thus be correlated, and by treating the whole burst of pulses in one operation, the data processor can separate the echo into strips arranged across the track by exploiting the slight frequency shifts (caused by the Doppler effect) in the forward- and aft-looking parts of the beam.
– SAR interferometer (SarIn) mode
In order to measure the arrival angle, a second receive antenna will be activated so that the radar echo is received by two antennas simultaneously. When the echo comes from a point not directly beneath the satellite there will be a difference in the path-length of the radar wave, which will be measured. Simple geometry will provide the angle between the baseline joining the antennas and the echo direction.
The location systems onboard Cryosat-2 will complement each other to measure the satellite’s position on orbit to within two centimetres on the radial component. The LRR is highly accurate but it requires ground stations that are complex to operate, and its use can be restricted by adverse weather conditions. It is used to calibrate DORIS measurements in order to determine the orbit in real time and to support precise orbit determination.
DORIS (Doppler location)
The DORIS system uses a ground network of orbitography beacons spread around the globe, which send signals at two frequencies to a receiver on the satellite. The relative motion of the satellite generates a shift in the signal’s frequency (called the Doppler shift) that is measured to derive the satellite’s velocity. These data are then assimilated in orbit determination models to keep permanent track of the satellite’s precise position (to within three centimetres) on its orbit.
LRR (laser tracking)
The LRR is an array of mirrors that provide a target for laser tracking measurements from the ground. By analysing the round-trip time of the laser beam, we can locate where the satellite is on its orbit.