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CRRESThe Combined Release and Radiation Effects SatelliteThe missionThe CRRES spacecraft was launched on 25th July 1990 to study the near-Earth space environment and the effects of the Earth's radiation environment on microelectronic components. It operated in a highly elliptical geosynchronous transfer orbit with a perigee of 305 km and an apogee of 35,768 km and an inclination of 18 degrees. The orbital period was 9 hours and 52 minutes and the initial apogee was at a magnetic local time of 08:00 MLT. The satellite thus swept through the heart of the radiation belts on average approximately 5 times per day, providing gopod coverage of this important region. Science ObjectivesThe three primary mission objectives were:
The Low Energy Plasma Analyser (LEPA) instrument consisted of two electrostatic analysers with microchannel plate detectors, each with a field of view of 120 degrees by 5 degrees, one measuring electrons, the other ions in the energy range 100 eV < E < 30 keV. The analysers were mounted on the spacecraft with the 120 degree range covering angles from 30 degrees to 150 degrees with respect to the spacecraft spin axis, the total range being divided intop 15 zones 8 degrees wide. The energy range was swept through the complete range 64 times per spin, synchronised to the spin period of 30 s. The instrument detected the complete pitch angle range from 0 degrees to 180 degrees every 30 s with a resolution of 5.625 x 8 degrees at all energies in the range 100 eV < E < 30 keV. The detailed pitch-angle distributions provided by the LEPA instrument have been used (and continue to be used) succesfully in a number of investigations including:-
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7th August 2000
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