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Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout
Research article (Advances in Space Research, 2020) · cited 15× · AI/ML
Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout
Summary
Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout is a scholarly article[1].
Key Facts
Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout's instance of is recorded as scholarly article[2].
References
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APA4ort.xyz Knowledge Graph. (2026). Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout. Retrieved May 24, 2026, from https://4ort.xyz/entity/feasibility-analysis-of-leo-and-geo-large-space-debris-de-re-orbiting-taking-into-account-launch-mass-of-spacecraft-coll
MLA“Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/feasibility-analysis-of-leo-and-geo-large-space-debris-de-re-orbiting-taking-into-account-launch-mass-of-spacecraft-coll.
BibTeX@misc{4ortxyz_feasibility-analysis-of-leo-and-geo-large-space-debris-de-re-orbiting-taking-into-account-launch-mass-of-spacecraft-coll_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout}}, year = {2026}, url = {https://4ort.xyz/entity/feasibility-analysis-of-leo-and-geo-large-space-debris-de-re-orbiting-taking-into-account-launch-mass-of-spacecraft-coll}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Feasibility analysis of LEO and GEO large space debris de/re-orbiting taking into account launch mass of spacecraft-collector and its configuration layout — https://4ort.xyz/entity/feasibility-analysis-of-leo-and-geo-large-space-debris-de-re-orbiting-taking-into-account-launch-mass-of-spacecraft-coll (retrieved 2026-05-24)
