The RADiation–hard Electron Monitor (RADEM) is an instrument on board the ESA JUpiter ICy moons Explorer (JUICE) deep-space mission launched on April 14th, 2023. As a part of the Cosmic Vision program, RADEM on JUICE will spend over three years exploring the radiation environment of the Jovian system, including its icy moons Ganymede, Callisto, and Europa. The instrument serves as an on-board radiation monitor, providing nonstop information on particle fluxes and their energy spectra. In addition to being a platform subsystem relevant to spacecraft safety and health, RADEM obtains scientifically valuable data on the radiation environment and extends the particle detection range covered by the JUICE Particle Environment Package (PEP) instrument suite to much higher energies, and broadens the energy coverage in the tens to hundreds of MeV range for electrons and protons, compared to past missions. RADEM consists of three detector subunits: the Electron Detector Head, the Proton & Heavy Ion Detector Head, and the Directional Detector Head. Each of them is connected to a separate readout electronics with a dedicated front-end Application–Specific Integrated Circuit (ASIC) designed especially for the JUICE mission. RADEM measures electrons in the 0.3–40 MeV energy range, protons in the 5–250 MeV energy range, and heavy ions within the Linear Energy Transfer range from 0.1 to 10 MeV cm mg−1. The Directional Detector provides an angular coverage of incoming radiation up to about 35% of the sky. Being a platform device, the monitor operates and delivers data permanently. Therefore, RADEM measurements also cover the radiation environment of the interplanetary space during the mission cruise phase, including long-term studies of the environment between Venus and Mars as well as the detection of the Solar Energetic Particle events that propagate across different locations in the Solar System.

Despite the growing importance of planetary Space Weather forecasting and radiation protection for science and robotic exploration and the need for accurate Space Weather monitoring and predictions, only a limited number of spacecraft have dedicated instrumentation for this purpose. However, every spacecraft (planetary or astronomical) has hundreds of housekeeping sensors distributed across the spacecraft, some of which can be useful to detect radiation hazards produced by solar particle events. In particular, energetic particles that impact detectors and subsystems on a spacecraft can be identified by certain housekeeping sensors, such as the Error Detection and Correction (EDAC) memory counters, and their effects can be assessed. These counters typically have a sudden large increase in a short time in their error counts that generally match the arrival of energetic particles to the spacecraft. We investigate these engineering datasets for scientific purposes and perform a feasibility study of solar energetic particle event detections using EDAC counters from seven European Space Agency Solar System missions: Venus Express, Mars Express, ExoMars-Trace Gas Orbiter, Rosetta, BepiColombo, Solar Orbiter, and Gaia. Six cases studies, in which the same event was observed by different missions at different locations in the inner Solar System are analyzed. The results of this study show how engineering sensors, for example, EDAC counters, can be used to infer information about the solar particle environment at each spacecraft location. Therefore, we demonstrate the potential of the various EDAC to provide a network of solar particle detections at locations where no scientific observations of this kind are available.