Editorial: Space environment characterization

Abstract

The space environment poses many challenges to spacecraft operations in Earth’s orbits. The environment is composed of various factors that must be taken into account, such as micrometeoroids and orbital debris (MMOD), space weather events, and harsh thermal and radiation conditions. Therefore, a thorough understanding of these factors and the ability to effectively address them is essential for the design, operation, and performance of spacecraft in Earth’s orbits. Space-based sensors and detectors are a growing trend that enables real-time measurements and observations of the space environment. The article by Dignam et al. discussed in this Research Topic presents a new design for a passive space dust detector intended for deployment in Low Earth Orbit (LEO) for roughly 1 year. Upon its return to Earth, the detector will be analyzed for impact features generated by dust particles. The detector design includes using multiple Kapton foils, which have been demonstrated to effectively preserve details of the impacting particles’ size and chemistry. The residue chemistry can be used to determine their origin (whether it is from human-made debris or naturally occurring micrometeoroids). The study also found that a thin coating of 10 nm of palladium effectively reduces the loss of mass on Kapton foils when exposed to atomic oxygen. A novel method of in-situ space debris detection was proposed in the article by Fexer that uses a combination of conductance and characteristic impedance measurements, enabling the detection of multiple small impacts along one line. In addition, this proposed system can be used in conjunction with existing detection methods, providing an additional level of redundancy. The use of CubeSats satellites as cost-efficient platforms for MMOD characterization is a new and promising approach. The article by Oikonomidou et al. describes the current progress of the MOVE-III CubeSat project at the Technical University of Munich, which focuses on obtaining in-situ measurements of sub-millimetre space debris and meteoroids in the Low Earth Orbit. The data collected on flux, particle mass, and velocity will be used to verify and enhance existing models for space debris. OPEN ACCESS