Abstract
Space debris has been acknowledged as one of the most significant issues facing the space industry, with efforts now being focused on controlling this problem before it is too late. Current solutions involve expendable single-use vehicles designed to deorbit large pieces of debris. This project aims to develop the structural design of a reusable spacecraft to remove collections of small space debris that will remain undamaged by launch conditions. To annihilate space debris on-site without needing a collection system or earth re-entry for disposing of them. The NIRCSAT-X project proposes a novel technique for space debris removal on-site to reduce cost. The NIRCSAT-X project aims to develop novel technology on the TRL-3 or TRL-4 level. The project aims at a continuous space debris removal system. The paper will present the development of the novel design's mechanical and thermal subsystems.
Original language | English |
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Title of host publication | Applications of remote sensing and GIS based on an innovative vision. Proceeding of The First International Conference of Remote Sensing and Space Sciences Applications, Egypt 2022 |
Editors | Abd Alla Gad, Dalia Elfiky, Abdelazim Negm, Salwa Elbeih |
Publisher | Springer Nature US |
Pages | 31-37 |
Number of pages | 7 |
ISBN (Electronic) | 9783031404474 |
ISBN (Print) | 9783031404467 |
DOIs | |
Publication status | Published - 04 Nov 2023 |
Publication series
Name | Springer Proceedings in Earth and Environmental Sciences |
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Volume | Part F1684 |
ISSN (Print) | 2524-342X |
ISSN (Electronic) | 2524-3438 |
Bibliographical note
Publisher Copyright:© The Author(s), under exclusive license to Springer Nature Switzerland AG 2023.
Keywords
- Finite element
- LEO
- Space debris
- Thermal desktop
- Thermal plasma
ASJC Scopus subject areas
- Oceanography
- Environmental Science (miscellaneous)
- Geophysics
- Earth and Planetary Sciences (miscellaneous)