PL3396300T3 - Urządzenie uruchamiające do odrzucania co najmniej jednej odłączalnej części pocisku, w szczególności czepca pocisku - Google Patents
Urządzenie uruchamiające do odrzucania co najmniej jednej odłączalnej części pocisku, w szczególności czepca pociskuInfo
- Publication number
- PL3396300T3 PL3396300T3 PL18290030T PL18290030T PL3396300T3 PL 3396300 T3 PL3396300 T3 PL 3396300T3 PL 18290030 T PL18290030 T PL 18290030T PL 18290030 T PL18290030 T PL 18290030T PL 3396300 T3 PL3396300 T3 PL 3396300T3
- Authority
- PL
- Poland
- Prior art keywords
- fairing
- missile
- ejecting
- actuating device
- removable part
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Actuator (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1700467A FR3065798A1 (fr) | 2017-04-28 | 2017-04-28 | Dispositif d'actionnement pour l'ejection d'au moins une partie amovible de missile, en particulier d'une coiffe |
EP18290030.8A EP3396300B1 (fr) | 2017-04-28 | 2018-04-10 | Dispositif d'actionnement pour l'éjection d'au moins une partie amovible de missile, en particulier d'une coiffe |
Publications (1)
Publication Number | Publication Date |
---|---|
PL3396300T3 true PL3396300T3 (pl) | 2020-06-29 |
Family
ID=60019937
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL18290030T PL3396300T3 (pl) | 2017-04-28 | 2018-04-10 | Urządzenie uruchamiające do odrzucania co najmniej jednej odłączalnej części pocisku, w szczególności czepca pocisku |
Country Status (8)
Country | Link |
---|---|
US (1) | US10942015B2 (pl) |
EP (1) | EP3396300B1 (pl) |
JP (1) | JP7029470B2 (pl) |
ES (1) | ES2775446T3 (pl) |
FR (1) | FR3065798A1 (pl) |
IL (1) | IL269773B2 (pl) |
PL (1) | PL3396300T3 (pl) |
WO (1) | WO2018197760A1 (pl) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112284196B (zh) * | 2020-12-25 | 2021-04-13 | 星河动力(北京)空间科技有限公司 | 用于运载火箭的整流罩分离系统及运载火箭 |
CN113513951A (zh) * | 2021-04-30 | 2021-10-19 | 中国工程物理研究院总体工程研究所 | 全包对开式头罩的连接解锁与防热系统 |
CN113551565B (zh) * | 2021-09-18 | 2021-11-30 | 中国科学院力学研究所 | 一种级间段气动保形的固体火箭及分离方法 |
FR3138203A1 (fr) * | 2022-07-21 | 2024-01-26 | Safran Electronics & Defense | Véhicule aérien à optique frontale protégée. |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5235128A (en) * | 1991-04-18 | 1993-08-10 | Loral Corporation | Separable missile nosecap |
JP3770430B2 (ja) * | 1997-06-30 | 2006-04-26 | 株式会社アイ・エイチ・アイ・エアロスペース | 飛翔体のノーズフェアリング分離装置 |
US7082878B2 (en) * | 2003-07-01 | 2006-08-01 | Raytheon Company | Missile with multiple nosecones |
DE102005030090B4 (de) * | 2005-06-27 | 2007-03-22 | Diehl Bgt Defence Gmbh & Co. Kg | Abwerfbare Vorsatzhaube sowie Flugkörper mit abwerfbarer Vorsatzhaube |
IL189089A0 (en) * | 2008-01-28 | 2008-08-07 | Rafael Advanced Defense Sys | Apparatus and method for splitting and removing a shroud from an airborne vehicle |
FR2947808B1 (fr) | 2009-07-09 | 2011-12-09 | Astrium Sas | Dispositif de separation lineaire douce d'une premiere piece et d'une seconde piece |
FR2966919B1 (fr) * | 2010-10-29 | 2013-11-01 | Tda Armements Sas | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. |
FR3022885B1 (fr) | 2014-06-25 | 2016-10-21 | Mbda France | Paroi structurante de missile, en particulier pour coiffe de protection thermique |
-
2017
- 2017-04-28 FR FR1700467A patent/FR3065798A1/fr not_active Withdrawn
-
2018
- 2018-04-10 EP EP18290030.8A patent/EP3396300B1/fr active Active
- 2018-04-10 JP JP2019554635A patent/JP7029470B2/ja active Active
- 2018-04-10 US US16/500,486 patent/US10942015B2/en active Active
- 2018-04-10 WO PCT/FR2018/000078 patent/WO2018197760A1/fr active Application Filing
- 2018-04-10 PL PL18290030T patent/PL3396300T3/pl unknown
- 2018-04-10 IL IL269773A patent/IL269773B2/en unknown
- 2018-04-10 ES ES18290030T patent/ES2775446T3/es active Active
Also Published As
Publication number | Publication date |
---|---|
US20200109929A1 (en) | 2020-04-09 |
IL269773A (en) | 2019-11-28 |
EP3396300B1 (fr) | 2019-12-25 |
IL269773B2 (en) | 2024-04-01 |
FR3065798A1 (fr) | 2018-11-02 |
IL269773B1 (en) | 2023-12-01 |
US10942015B2 (en) | 2021-03-09 |
WO2018197760A1 (fr) | 2018-11-01 |
JP7029470B2 (ja) | 2022-03-03 |
ES2775446T3 (es) | 2020-07-27 |
EP3396300A1 (fr) | 2018-10-31 |
JP2020517882A (ja) | 2020-06-18 |
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