WO2026005740 - MISSILE USING ENERGY SOURCE CHARGED IN THE LAUNCHER
National phase entry is expected:
Publication Number
WO/2026/005740
Publication Date
02.01.2026
International Application No.
PCT/TR2025/050652
International Filing Date
23.06.2025
Title **
[English]
MISSILE USING ENERGY SOURCE CHARGED IN THE LAUNCHER
[French]
MISSILE UTILISANT UNE SOURCE D'ÉNERGIE CHARGÉE DANS LE LANCEUR
Applicants **
ROKETSAN ROKET SANAYİİ TİCARET A.Ş.
Inventors
GÜNÇAN, Ali Murat
Priority Data
2024/007974
24.06.2024
TR
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
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| Number of Multi-Dependent Claims | * |
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International Searching Authority |
Turkpatent
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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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| Entry into National Phase under |
Chapter I
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| Patent Delivery |
Send the Letters Patent by Courier
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| 译文 |
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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 | 1958 | |
| EPO | Filing, Examination, Granting | 9151 | |
| Japan | Filing, Examination, Granting | 1968 | |
| South Korea | Filing, Examination, Granting | 1735 | |
| USA | Filing, Examination, Granting | 4740 |
Total:
19,552
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Abstract[English]
The invention relates to a missile system (100) that consists of a missile (120) that is charged before launch and instead of a thermal battery, has an optimised energy source (130) with a voltage boost circuit (132) and voltage buck circuit (133), and launcher (110) containing power unit (113) to charge/discharge energy source (130) in order to reduce costs and increase efficiency.[French]
L'invention concerne un système de missile (100) qui est constitué d'un missile (120) qui est chargé avant le lancement et au lieu d'une batterie thermique, a une source d'énergie (130) optimisée avec un circuit d'amplification de tension (132) et un circuit abaisseur de tension (133), et un lanceur (110) contenant une unité d'alimentation (113) pour charger/décharger une source d'énergie (130) afin de réduire les coûts et d'augmenter l'efficacité.