FR2966919B1 - Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. - Google Patents
Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe.Info
- Publication number
- FR2966919B1 FR2966919B1 FR1004269A FR1004269A FR2966919B1 FR 2966919 B1 FR2966919 B1 FR 2966919B1 FR 1004269 A FR1004269 A FR 1004269A FR 1004269 A FR1004269 A FR 1004269A FR 2966919 B1 FR2966919 B1 FR 2966919B1
- Authority
- FR
- France
- Prior art keywords
- munition
- nosecone
- guided
- pyrotechnic
- munition body
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/38—Constructions adapted to reduce effects of aerodynamic or other external heating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Automotive Seat Belt Assembly (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1004269A FR2966919B1 (fr) | 2010-10-29 | 2010-10-29 | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. |
US13/882,398 US20130264425A1 (en) | 2010-10-29 | 2011-10-25 | Separable streamlined nose cone for a guided munition, and guided munition including such a nose cone |
EP11775941.5A EP2633261A1 (fr) | 2010-10-29 | 2011-10-25 | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe |
PCT/EP2011/068688 WO2012059369A1 (fr) | 2010-10-29 | 2011-10-25 | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. |
IL226021A IL226021A0 (en) | 2010-10-29 | 2013-04-28 | A current separable nose cone for guiding ammunition, and guided ammunition containing such a nose cone |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1004269A FR2966919B1 (fr) | 2010-10-29 | 2010-10-29 | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2966919A1 FR2966919A1 (fr) | 2012-05-04 |
FR2966919B1 true FR2966919B1 (fr) | 2013-11-01 |
Family
ID=44080272
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1004269A Active FR2966919B1 (fr) | 2010-10-29 | 2010-10-29 | Coiffe aerodynamique secable pour munition guidee et munition guidee comportant une telle coiffe. |
Country Status (5)
Country | Link |
---|---|
US (1) | US20130264425A1 (fr) |
EP (1) | EP2633261A1 (fr) |
FR (1) | FR2966919B1 (fr) |
IL (1) | IL226021A0 (fr) |
WO (1) | WO2012059369A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3065798A1 (fr) * | 2017-04-28 | 2018-11-02 | Mbda France | Dispositif d'actionnement pour l'ejection d'au moins une partie amovible de missile, en particulier d'une coiffe |
FR3138203A1 (fr) * | 2022-07-21 | 2024-01-26 | Safran Electronics & Defense | Véhicule aérien à optique frontale protégée. |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3070018A (en) * | 1961-02-27 | 1962-12-25 | Marcellus W Fahi | Nose cone ejection system |
US3362290A (en) * | 1965-04-13 | 1968-01-09 | Mc Donnell Douglas Corp | Non-contaminating thrusting separation system |
US3453960A (en) * | 1967-12-11 | 1969-07-08 | Gen Dynamics Corp | Noncontaminating linear explosive separation |
US3601055A (en) * | 1969-02-25 | 1971-08-24 | Us Navy | Protective nose cover and in-flight removal means |
US3674227A (en) * | 1970-03-23 | 1972-07-04 | Hughes Aircraft Co | Fragmenting cover |
US3706281A (en) * | 1971-04-01 | 1972-12-19 | Nasa | Method and system for ejecting fairing sections from a rocket vehicle |
DE3638847C1 (de) * | 1986-11-13 | 1996-07-25 | Bodenseewerk Geraetetech | Flugkörperbaugruppe mit strahlungsdurchlässigem Abdeckkörper und Fassungsring |
US4699062A (en) * | 1987-02-11 | 1987-10-13 | The United States Of America As Represented By The Secretary Of The Navy | VLA (alwt) airframe clamshell opener assembly |
US5167386A (en) * | 1992-01-21 | 1992-12-01 | Rockwell International Corporation | Pyrotechnic removal of a radome cover |
DE4235266C1 (de) * | 1992-10-20 | 1993-10-21 | Bodenseewerk Geraetetech | Verbindungsanordnung zum Verbinden eines einen Suchkopf abdeckenden Domes mit der Struktur eines Flugkörpers |
DE10240040A1 (de) * | 2002-08-27 | 2004-03-11 | BODENSEEWERK GERäTETECHNIK GMBH | Lenkflugkörper mit abwerfbarer Schutzkappe |
IL167905A (en) * | 2005-04-07 | 2008-06-05 | Israel Aerospace Ind Ltd | Structure coupler and coupler therefor |
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 |
FR2966920B1 (fr) * | 2010-10-29 | 2013-05-17 | Tda Armements Sas | Coiffe aerodynamique ejectable pour munition guidee et munition guidee comportant une telle coiffe. |
US8497456B2 (en) * | 2011-03-30 | 2013-07-30 | Raytheon Company | Guided munitions including interlocking dome covers and methods for equipping guided munitions with the same |
-
2010
- 2010-10-29 FR FR1004269A patent/FR2966919B1/fr active Active
-
2011
- 2011-10-25 EP EP11775941.5A patent/EP2633261A1/fr not_active Withdrawn
- 2011-10-25 US US13/882,398 patent/US20130264425A1/en not_active Abandoned
- 2011-10-25 WO PCT/EP2011/068688 patent/WO2012059369A1/fr active Application Filing
-
2013
- 2013-04-28 IL IL226021A patent/IL226021A0/en unknown
Also Published As
Publication number | Publication date |
---|---|
EP2633261A1 (fr) | 2013-09-04 |
FR2966919A1 (fr) | 2012-05-04 |
IL226021A0 (en) | 2013-06-27 |
WO2012059369A1 (fr) | 2012-05-10 |
US20130264425A1 (en) | 2013-10-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CL | Concession to grant licences |
Name of requester: L'ETAT FRANCAIS, FR Effective date: 20150318 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |