Author/Authors :
Maddox، نويسنده , , Erik and Palacios، نويسنده , , Alex and Lampridis، نويسنده , , Dimitris and Kraft، نويسنده , , Stefan and Owens، نويسنده , , Alan and Tomuta، نويسنده , , Dana and Ostendorf، نويسنده , , Reint، نويسنده ,
Abstract :
For future exploration of the solar system, the European Space Agency (ESA) is planning missions to Mercury (BepiColombo), the Sun (SolarOrbiter) and to the moons of Jupiter and Saturn. The expected intensity of radiation during such missions is hazardous for the scientific instruments and the satellite. To extend the lifetime of the satellite and its payload a multifunctional particle spectrometer (MPS) is being developed. The basic function of the MPS is to send an alarm signal to the satellite control system during periods of high radiation. In addition the MPS is a scientific instrument that will unfold the composition of the different contributing particles on-line by the dE/dx versus E method. The energy spectrum and angular distribution of the particles will be recorded as well. This article describes the main requirements and the base line design for the MPS. A readout scheme consisting of a 32 channel ASIC from IDEAS is proposed and the signal filtering algorithm will run on a digital signal processor based on FPGA technology. Results are shown from prototype calibration studies with a proton beam.
Keywords :
Planetary exploration , Particle identification , FPGA , Radiation monitor , Instrument calibration