FR2960055B1 - Munition guidee protegee par une coiffe aerodynamique - Google Patents
Munition guidee protegee par une coiffe aerodynamiqueInfo
- Publication number
- FR2960055B1 FR2960055B1 FR1002024A FR1002024A FR2960055B1 FR 2960055 B1 FR2960055 B1 FR 2960055B1 FR 1002024 A FR1002024 A FR 1002024A FR 1002024 A FR1002024 A FR 1002024A FR 2960055 B1 FR2960055 B1 FR 2960055B1
- Authority
- FR
- France
- Prior art keywords
- coiffe
- aerodynamic
- protected
- guided munition
- munition
- 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
-
- 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
- F42B15/01—Arrangements thereon for guidance or control
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1002024A FR2960055B1 (fr) | 2010-05-12 | 2010-05-12 | Munition guidee protegee par une coiffe aerodynamique |
PCT/EP2011/057648 WO2011141527A1 (fr) | 2010-05-12 | 2011-05-11 | Munition guidee protegee par une coiffe aerodynamique |
US13/697,301 US20130193264A1 (en) | 2010-05-12 | 2011-05-11 | Guided Munitions Protected by an Aerodynamic Cap |
JP2013509566A JP2013530367A (ja) | 2010-05-12 | 2011-05-11 | 空気力学的弾頭冠により保護された誘導兵器 |
EP11719013A EP2569591A1 (fr) | 2010-05-12 | 2011-05-11 | Munition guidee protegee par une coiffe aerodynamique |
IL222976A IL222976A0 (en) | 2010-05-12 | 2012-11-11 | Guided munition protected by an aerodynamic cap |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1002024A FR2960055B1 (fr) | 2010-05-12 | 2010-05-12 | Munition guidee protegee par une coiffe aerodynamique |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2960055A1 FR2960055A1 (fr) | 2011-11-18 |
FR2960055B1 true FR2960055B1 (fr) | 2015-11-20 |
Family
ID=43413870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1002024A Active FR2960055B1 (fr) | 2010-05-12 | 2010-05-12 | Munition guidee protegee par une coiffe aerodynamique |
Country Status (6)
Country | Link |
---|---|
US (1) | US20130193264A1 (fr) |
EP (1) | EP2569591A1 (fr) |
JP (1) | JP2013530367A (fr) |
FR (1) | FR2960055B1 (fr) |
IL (1) | IL222976A0 (fr) |
WO (1) | WO2011141527A1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014011035A1 (de) * | 2014-07-23 | 2016-01-28 | Diehl Bgt Defence Gmbh & Co. Kg | Rumpfbughaube für einen Flugkörper |
US10809045B1 (en) | 2018-05-10 | 2020-10-20 | The United States Of America As Represented By The Secretary Of The Air Force | Forward firing fragmentation (FFF) munition including fragmentation adjustment system and associated methods |
US10928169B2 (en) * | 2019-02-07 | 2021-02-23 | Bae Systems Rokar International Ltd. | Seal for a projectile guiding kit |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2782716A (en) * | 1953-11-30 | 1957-02-26 | North American Aviation Inc | Destructible cover for fragile dome |
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 |
US3970006A (en) * | 1975-01-16 | 1976-07-20 | The United States Of America As Represented By The Secretary Of The Air Force | Protective cover for a missile nose cone |
US4301708A (en) * | 1979-07-25 | 1981-11-24 | The United States Of America As Represented By The Secretary Of The Navy | Launch tube closure |
CH644447A5 (de) * | 1980-04-22 | 1984-07-31 | Oerlikon Buehrle Ag | Leuchtrakete mit zylindrischem behaelter. |
US5457471A (en) * | 1984-09-10 | 1995-10-10 | Hughes Missile Systems Company | Adaptively ablatable radome |
US4753169A (en) * | 1985-12-23 | 1988-06-28 | General Dynamics, Pomona Division | Ablating electromagnetic shield sheath |
US5159151A (en) * | 1986-05-08 | 1992-10-27 | British Aerospace Public Limited Company | Missile nose fairing assembly |
US4797683A (en) * | 1986-10-01 | 1989-01-10 | United Technologies Corporation | Multi-spectral radome |
US4867357A (en) * | 1987-12-21 | 1989-09-19 | General Dynamics Corp., Pomona Division | Jettisonable protective cover device |
US5408244A (en) * | 1991-01-14 | 1995-04-18 | Norton Company | Radome wall design having broadband and mm-wave characteristics |
US5125600A (en) * | 1991-06-03 | 1992-06-30 | Rockwell International Corporation | Removable radome cover |
US5167386A (en) * | 1992-01-21 | 1992-12-01 | Rockwell International Corporation | Pyrotechnic removal of a radome cover |
FR2702273B1 (fr) * | 1993-03-05 | 1995-06-02 | Lacroix E Tous Artifices | Tête pyrotechnique à moyens de dispersion perfectionnés. |
JPH09196599A (ja) * | 1996-01-23 | 1997-07-31 | Mitsubishi Heavy Ind Ltd | 飛しょう体のシーカドーム |
DE10240040A1 (de) * | 2002-08-27 | 2004-03-11 | BODENSEEWERK GERäTETECHNIK GMBH | Lenkflugkörper mit abwerfbarer Schutzkappe |
DE102004053449B4 (de) * | 2004-11-05 | 2010-12-09 | Diehl Bgt Defence Gmbh & Co. Kg | Vorsatzhaube |
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 |
US8519312B1 (en) * | 2010-01-29 | 2013-08-27 | Raytheon Company | Missile with shroud that separates in flight |
-
2010
- 2010-05-12 FR FR1002024A patent/FR2960055B1/fr active Active
-
2011
- 2011-05-11 US US13/697,301 patent/US20130193264A1/en not_active Abandoned
- 2011-05-11 EP EP11719013A patent/EP2569591A1/fr not_active Withdrawn
- 2011-05-11 JP JP2013509566A patent/JP2013530367A/ja not_active Withdrawn
- 2011-05-11 WO PCT/EP2011/057648 patent/WO2011141527A1/fr active Application Filing
-
2012
- 2012-11-11 IL IL222976A patent/IL222976A0/en unknown
Also Published As
Publication number | Publication date |
---|---|
WO2011141527A1 (fr) | 2011-11-17 |
FR2960055A1 (fr) | 2011-11-18 |
US20130193264A1 (en) | 2013-08-01 |
IL222976A0 (en) | 2013-02-03 |
JP2013530367A (ja) | 2013-07-25 |
EP2569591A1 (fr) | 2013-03-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |