WO2023161717 - SPACE VEHICLE THERMAL MANAGEMENT SYSTEM AND METHOD FOR MANUFACTURE THEREOF
National phase entry:
Publication Number
WO/2023/161717
Publication Date
31.08.2023
International Application No.
PCT/IB2023/000100
International Filing Date
24.02.2023
Title **
[English]
SPACE VEHICLE THERMAL MANAGEMENT SYSTEM AND METHOD FOR MANUFACTURE THEREOF
[French]
SYSTÈME DE GESTION THERMIQUE DE VÉHICULE SPATIAL ET SON PROCÉDÉ DE FABRICATION
Applicants **
NETWORK ACCESS ASSOCIATES LIMITED
Inventors
COLAS, Victor
NAGI, Manraj
Priority Data
FR2201685
25.02.2022
FR
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
| Number of Priorities | * |
| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
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| Number of Pages with Drawings | * |
| Pages of Specification | * |
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| Number of Office Actions | * |
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International Searching Authority |
EPO
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| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
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| Type of Assignment |
The Standard Agent's Assignment
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| Applicant's Legal Status |
Legal Entity
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| * | |
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| Entry into National Phase under |
Chapter I
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| Patent Delivery |
Send the Letters Patent by Courier
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| Translation |
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* The data is based on automatic recognition. Please verify and amend if necessary.
** 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 | 1082 | |
| EPO | Filing, Examination, Granting | 7669 | |
| Japan | Filing, Examination, Granting | 1609 | |
| South Korea | Filing, Examination, Granting | 1095 | |
| USA | Filing, Examination, Granting | 3490 |
Total:
14,945
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 vehicle includes a first aluminum panel, a second aluminum panel fixed to the first aluminum panel around at least a portion of respective perimeters thereof to thereby form an enclosed structure having an interior volume, a plurality of grooves formed in at least one of the first aluminum panel or the second aluminum panel, at least one heat transport element positioned in at least one of the plurality of grooves, and a plurality of onboard equipment elements, where at least one of the plurality of onboard equipment elements is positioned adjacent to the heat transport element, where at least some of the plurality of onboard equipment elements lack a casing, and where the at least one heat transport element is configured to transport heat away from the plurality of onboard equipment elements.[French]
L'invention concerne un véhicule spatial comprenant un premier panneau d'aluminium, un second panneau d'aluminium fixé au premier panneau d'aluminium autour d'au moins une partie de leurs périmètres respectifs pour former ainsi une structure fermée ayant un volume intérieur, une pluralité de rainures formées dans le premier panneau d'aluminium et/ou le second panneau d'aluminium, au moins un élément de transport de chaleur positionné dans au moins l'une de la pluralité de rainures, et une pluralité d'éléments d'équipement embarqués, au moins l'un de la pluralité d'éléments d'équipement embarqué étant positionné adjacent à l'élément de transport de chaleur, au moins certains de la pluralité d'éléments d'équipement embarqués étant dépourvus d'un boîtier, et le ou les éléments de transport de chaleur étant configurés pour transporter la chaleur à l'opposé de la pluralité d'éléments d'équipement embarqués.