WO2024171157 - SPACE DEBRIS DETECTION AND MITIGATION WITH A NETWORK OF DEPLOYED OBSERVATORIES
National phase entry is expected:
Publication Number
WO/2024/171157
Publication Date
22.08.2024
International Application No.
PCT/IB2024/051532
International Filing Date
17.02.2024
Title **
[English]
SPACE DEBRIS DETECTION AND MITIGATION WITH A NETWORK OF DEPLOYED OBSERVATORIES
[French]
DÉTECTION ET ATTÉNUATION DE DÉBRIS SPATIAUX AVEC UN RÉSEAU D'OBSERVATOIRES DÉPLOYÉS
Applicants **
SOUTHERN CROSS OUTREACH OBSERVATORY PROJECT (SCOOP)
HUSSAIN, Muhammad Akbar
HUSSAIN, Muhammad Mehdi
HAIDER, Muhammad Waqar
HUSSAIN, Muhammad Ayaz
Inventors
HUSSAIN, Muhammad Akbar
HUSSAIN, Muhammad Mehdi
HAIDER, Muhammad Waqar
HUSSAIN, Muhammad Ayaz
Priority Data
63/485,679
17.02.2023
US
Application details
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** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 2086 | |
| EPO | Filing, Examination, Granting | 10982 | |
| Japan | Filing, Examination, Granting | 2183 | |
| South Korea | Filing, Examination, Granting | 1654 | |
| USA | Filing, Examination, Granting | 4740 |
Total:
21,645
The term for entry into the National Phase has expired. This quotation is for informational purposes only
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Abstract[English]
A space debris removing device, system and method are disclosed. The system comprises a central server, a primary detection node, at least two secondary tracer nodes, the central server is configured to assign a tertiary node to track the debris with laser, wherein the tertiary node is configured to mark the debris being tracked with the laser, creating a laser illuminated target (LIT), a tertiary tracking unit deployed at the tertiary node, and a ground-based kilowatt laser system configured to pick up the LIT by using one or more optical sensors and tackle the debris with a high power laser beam.[French]
L'invention concerne un dispositif, un système et un procédé d'élimination de débris spatiaux. Le système comprend un serveur central, un nœud de détection primaire, au moins deux nœuds traceurs secondaires, le serveur central est configuré pour attribuer un nœud tertiaire pour suivre les débris avec un laser, le nœud tertiaire étant configuré pour marquer les débris qui sont suivis avec le laser, créer une cible éclairée par laser (LIT), une unité de suivi tertiaire déployée au niveau du nœud tertiaire, et un système laser de kilowatt basé au sol configuré pour capter la LIT à l'aide d'un ou de plusieurs capteurs optiques et attaquer les débris avec un faisceau laser haute puissance.