The article was originally published with attribution and spelling errors tied to two of its authors. The previously incorrect name, Alankritaa Mrigatshi, has been corrected to Alankrita Isha Mrigakshi and should be reflected as such in all versions of the article. The author’s affiliation details and email address have also been updated. In addition, the last name of Ingo Reinaecker has been corrected to Rienäcker, along with the corresponding update to the author’s email address. The original article has been corrected.

Additive manufacturing (AM) rapidly expands to all research areas due to its multiple advantages, such as the freedom and flexibility in achieving any geometry. Using AM as a fabrication technique, the design process has almost no limitations, blending considerably well with the irregular geometries that may result from topology optimization. Yet, in practice the application of AM together with topologically optimized geometries is not as straightforward. In this research, a hollow square t-joint is used as a case study to investigate and understand the difficulties in the design and manufacturing of steel parts using wire arc additive manufacturing (WAAM). The case study showcases from the application of two optimization methods with various parameters to find an optimal geometry; numerical analysis (FEM) on non-optimized and optimized models; a procedure called “re-engineering” that adjusts the optimized geometry to structure efficiency and AM effectiveness; dynamic slicing and path planning; an adjustment of the welding parameters to enhance the material properties and accuracy of the final specimens; and experimental assessments on non-optimized and optimized printed t-joints to validate the entire process. The application of this process allowed the manufacture of a complex optimized geometry, which have more resistance than the non-optimized T-joint.

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.

The component method for joint analysis relies on the formulation of stiffness and strength of individual parts to derive the global properties of the joint. One of these components is the web of an open I-section, or the face of a rectangular hollow section, hereby referred to as face plate. It is currently not codified despite its frequent occurrence in the engineering practice. Hereby, a new mechanical model is proposed to estimate the initial stiffness of the face plate component under out-of-plane loading, leading to closed-form analytical expressions. The model is validated against experimental test results and an extensive numerical parametric study, showing excellent agreement.