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 pocisku

Info

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
Application number
PL18290030T
Other languages
English (en)
Inventor
Clément Quertelet
Clyde Laheyne
Original Assignee
Mbda France
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mbda France filed Critical Mbda France
Publication of PL3396300T3 publication Critical patent/PL3396300T3/pl

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)
PL18290030T 2017-04-28 2018-04-10 Urządzenie uruchamiające do odrzucania co najmniej jednej odłączalnej części pocisku, w szczególności czepca pocisku PL3396300T3 (pl)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
JP2020517882A (ja) 2020-06-18
JP7029470B2 (ja) 2022-03-03
ES2775446T3 (es) 2020-07-27
FR3065798A1 (fr) 2018-11-02
US10942015B2 (en) 2021-03-09
EP3396300A1 (fr) 2018-10-31
IL269773B2 (en) 2024-04-01
US20200109929A1 (en) 2020-04-09
IL269773B1 (en) 2023-12-01
WO2018197760A1 (fr) 2018-11-01
IL269773A (en) 2019-11-28
EP3396300B1 (fr) 2019-12-25

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