Data from the following sensors are presented:


ERS -1,2 SAR
TU-134, AN-24 Aircraft RAR
SIR-C/X SAR
Ocean-7 RAR

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I. ERS-1, ERS-2 SAR

European Remote Sensing Satellite (ERS-1) was launched on 17 July 1991, and the follow mission ERS-2 (with the same sensors and an Ozone monitoring instrument added) was launched on 21 April 1995.

ERS-1 and ERS-2 satellites are in similar orbits.

The ERS-1 mission is split in several phases with different repeat cycles, optimized for different applications.

ERS-2 has a fixed repeat cycle of 35 days, and follows ERS-1 tracks with one day's delay.

AMI-SAR (Active Microwave Imager in Synthetic Aperture Radar) operates at C- band (5.3 GHz, 5.6 cm), 15.55 MHz bandwidth, VV-polarization, pulse repetition frequency 1640-1720 Hz, transmitted pulse length 64ns (compressed), transmitted peak power 4.8 kW. The physical antenna size is 10m x 1m. The incidence angle on the horizontal Earth surface at mid swath is 23 (ranging from 19 at near range to 26 at far range). Swath width is 102.5 km (telemetered), spatial resolution is about 25x25 m.


II. Ku-Band Real Aperture Radar on board aircraft laboratories AN-24, Tu-134

RADAR SYSTEM PARAMETERS

Ku-band (l=2.25 cm) real-aperture radar operating with the peak power of 60 kW,  the 2 kHz pulse repetition frequency and a 110 ns transmitted pulse-width.

Two cylindrical antennas, one on each side of the aircraft, transmit and receive alternate pulses of horizontal and vertical polarizations at large incident angles of 72-84 to produce simultaneous  HH and VV images.

The radar swath of 12.5 km is illuminated on each side of ground track. Spatial resolution is about 25x25 meters.
 


III. SIR-C/X SAR

The Spaceborne Imaging Radar-C/X-band Synthetic Radar (SIR-C/X-SAR), carried in the cargo bay of the Space Shuttle Endeavour in April and October of 1994, simultaneously recorded SAR data at three wavelengths (L-, C-, and X-bands; 23.5, 5.8, and 3.1 cm, respectively). In addition, the full polarimetric scattering matrix was obtained by the SIR-C instrument at L- and C-band over a variety of terrain and vegetation types. The integrated system is steerable in look angle (electronically in the case of SIR-C, mechanically in the case of X-SAR) to obtain data in the angular range of 15-16 Degree. Imaging resolution varies from about 10 to 50 meters, depending on the geometry and data taking configuration.

Over the two flights, a total of 143 hours (93 terabits) of SAR data were digitally recorded on tape for subsequent processing in the U.S., Germany, and Italy. During the October 1994 flight of SIR-C/X-SAR, over one million square kilometers of repeat-pass SAR interferometry data were also obtained.

SIR-C/X-SAR is a cooperative experiment between the NASA (National Aeronautics and Space Administration), the German space agency, DARA (Deutsche Agentur fur Raumfahrtangelegenheiten), and the Italian Space Agency, ASI (Agenzia Spaziale Italiana). SIR-C was developed by NASA's JPL (Jet Propulsion Laboratory). X-SAR was developed by the Dornier and Alenia Spazio companies, with the DLR (Deutsche Forschungsanstalt fur Luft- und Raumfahrt), the major partner in science, operations, and data processing.


IV. Ocean-7 RAR

Ocean-7 was launched in October 1994. It was developed at the Institute of Radiophysics and Electronics of the Ukrainian Academy of Sciences. Spatial resolution is 1-3 km within a swath of 460 km. The incidence angle changes from 21 to 46 within the swath. The RAR operates at a wavelength of 3.16 cm with vertical polarization.







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