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Description
Space radiation poses a threat not only to human space flight missions, but also to the electronic equipment of any space mission. Some dramatic space system failures and disturbances in recent years have been assumed to be radiation-induced malfunction of critical electronics parts. The space radiation environment consist of a variety of particle species, including electrons, protons and heavy ions, which may pose threats at different levels to different electronic devices. Therefore, the presence of a radiation monitor on-board of any mission is highly desirable to provide the capability to take protective measures in-flight and to contribute with flight-data to the improvement of existing radiation environment models. This contribution describes the development of a novel Miniaturized Radiation Monitor (MIRAM) for this purpose. Compared to the currently used devices, it is cheaper, has lower weight and power consumption. It is capable of providing a continuous measurement of dose as well as an estimation of the particle species composition of the radiation environment.
MIRAM has the dimensions 80 x 60 x 30 mm. It's nominal power consumption is 1.2 W with a peak consumption of 1.8 W. The device features four single pad diodes and a Timepix3 pixel detector with 256 x 256 pixels in a 55
The MIRAM device supports on-board analysis of the measured data to be able to work autonomously. The dose rate is calculated continuously based on the energy deposition in the Timepix3 detector. For the estimation of the particle species composition of the radiation environment, two methods are applied depending on the current flux. At lower fluxes (
Both methods have been developed with the help of reference measurements of monoenergetic electrons, protons and heavier ions of different energies on the ground in conjunction with measurement of the Space Application of Timepix Radiation Monitor (SATRAM), which measures the space radiation environment in a Low Earth Orbit (LEO) on-board the Proba-V satellite since 2013, in space. The measurements were supported by a Monte Carlo simulation of the MIRAM device.