Waldemar Bauer
Vitali Braun
Yukihiton Kitazawa
Igor Telichev- 1German Aerospace Center (DLR), Bremen, Germany
- 2European Space Agency (ESA), Darmstadt, Germany
- 3Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan
- 4Department of Mechanical Engineering, The University of Manitoba, Winnipeg, MB, Canada
Editorial on the Research Topic
Space environment characterization
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.
The article by Hanada et al. examines the potential of improving orbital debris (OD) models and presents analysis techniques for OD datasets. It has proposed a new approach to estimate the direction of angular momentum of a broken-up object at a specific time from in-situ debris measurements.
The article by Klein et al. discusses another aspect of the space environment, providing an in-depth analysis of proton radiation spectra. This research can potentially be beneficial for a wide range of space-related applications, including mission analysis and material and component development.
An accurate atmospheric density model and an atmospheric composition model are crucial for predicting orbits and controlling debris in LEO. The article by Kimoto et al. examines the data on atomic oxygen in super-low Earth orbit at an altitude of 300 km or less, obtained from the sensors installed onboard the SLATS satellite. The analysis of this data is expected to provide valuable insights into the material degradation caused by atomic oxygen on satellites operating in the super low Earth orbits.
We anticipate that this Research Topic will serve as a valuable resource for readers, providing an overview of the current state of the art in the rapidly developing field of space environment characterization.
Author contributions
IT wrote the initial draft of the editorial, reviews by WB, VB, and YK.
Conflict of interest
The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.
Publisher’s note
All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.
Keywords: space debris, meteoroids, space environment, in-situ debris measurement, modelling
Citation: Bauer W, Braun V, Kitazawa Y and Telichev I (2023) Editorial: Space environment characterization. Front. Space Technol. 4:1159825. doi: 10.3389/frspt.2023.1159825
Received: 06 February 2023; Accepted: 16 February 2023;
Published: 24 February 2023.
Edited and reviewed by:
Guglielmo S. Aglietti, The University of Auckland, New ZealandCopyright © 2023 Bauer, Braun, Kitazawa and Telichev. This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.
*Correspondence: Vitali Braun, dml0YWxpLmJyYXVuQGVzYS5pbnQ=