DE60306038D1 - Weapon containing a rocket mounted on a stealth plane, and weapon system containing a stealth plane and such a weapon - Google Patents
Weapon containing a rocket mounted on a stealth plane, and weapon system containing a stealth plane and such a weaponInfo
- Publication number
- DE60306038D1 DE60306038D1 DE60306038T DE60306038T DE60306038D1 DE 60306038 D1 DE60306038 D1 DE 60306038D1 DE 60306038 T DE60306038 T DE 60306038T DE 60306038 T DE60306038 T DE 60306038T DE 60306038 D1 DE60306038 D1 DE 60306038D1
- Authority
- DE
- Germany
- Prior art keywords
- weapon
- control units
- stealth
- tube
- plane
- 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.)
- Expired - Lifetime
Links
- 238000000926 separation method Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/06—Rocket or torpedo launchers for rockets from aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Heat Sensitive Colour Forming Recording (AREA)
Abstract
The system has first control units for separating the lower longitudinal part (7A) of the low radar signature tube from the top part (7B) which is connected to the external body of the aircraft (A) such that it creates in the tube, by its separation, an opening (8) allowing the complete ejection of the missile, with second control units (9) for controlling the first units, and third control units (10) controllable for movably connecting the missile when it is controlled, and fourth control units (11) for controlling the third control units. The weapon system is carried by a stealth aircraft, and has a low radar signature tube (4) which is radar absorbing, with a missile (M) located inside this tube.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0207632A FR2841333B1 (en) | 2002-06-20 | 2002-06-20 | WEAPON ARRANGED ON A FURTHER AIRCRAFT AND PROVIDED WITH A MISSILE, AND AN ARM SYSTEM COMPRISING A FURTHER AIRCRAFT AND A SUCH ARMY |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE60306038D1 true DE60306038D1 (en) | 2006-07-27 |
Family
ID=29717061
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE60306038T Expired - Lifetime DE60306038D1 (en) | 2002-06-20 | 2003-05-06 | Weapon containing a rocket mounted on a stealth plane, and weapon system containing a stealth plane and such a weapon |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP1375345B1 (en) |
| AT (1) | ATE329826T1 (en) |
| DE (1) | DE60306038D1 (en) |
| FR (1) | FR2841333B1 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ITRM20110626A1 (en) * | 2011-11-25 | 2013-05-26 | Aeronautical Service S R L | METHOD FOR THE REALIZATION OF SUPPORT SUPPORTS FOR AVIONICS. |
| DE102014004838A1 (en) | 2014-04-02 | 2015-10-08 | Airbus Defence and Space GmbH | Effector with discardable Tarnschale |
| US10086942B2 (en) | 2015-06-22 | 2018-10-02 | Bae Systems Plc | Aircraft stores transport system |
| EP3310661B1 (en) | 2015-06-22 | 2019-10-02 | BAE Systems PLC | Aircraft payload launch system |
| EP3109157A1 (en) * | 2015-06-22 | 2016-12-28 | BAE Systems PLC | Aircraft stores transport system |
| CN110530204B (en) * | 2019-07-17 | 2021-10-01 | 北京玻钢院复合材料有限公司 | Directional separating piece and directional separating structure of integrally-broken type launching box sealing cover |
| TR2022019965A1 (en) * | 2022-12-21 | 2024-07-22 | Tusas Tuerk Havacilik Ve Uzay Sanayii Anonim Sirketi | An ammunition storage element. |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5279199A (en) * | 1992-08-14 | 1994-01-18 | Hughes Aircraft Company | Technique and apparatus for rearward launch of a missile |
| US5717397A (en) * | 1996-05-17 | 1998-02-10 | Lockheed Martin Corporation | Low observable shape conversion for aircraft weaponry |
| FR2796454B1 (en) | 1999-07-16 | 2002-08-09 | Aerospatiale Matra Missiles | WEAPON MOUNTED ON A FURTIVE AIRCRAFT PROVIDED WITH A MISSILE, AS WELL AS A WEAPON SYSTEM COMPRISING A FURTIVE AIRCRAFT AND SUCH A WEAPON |
-
2002
- 2002-06-20 FR FR0207632A patent/FR2841333B1/en not_active Expired - Lifetime
-
2003
- 2003-05-06 AT AT03291082T patent/ATE329826T1/en not_active IP Right Cessation
- 2003-05-06 EP EP03291082A patent/EP1375345B1/en not_active Expired - Lifetime
- 2003-05-06 DE DE60306038T patent/DE60306038D1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| ATE329826T1 (en) | 2006-07-15 |
| FR2841333B1 (en) | 2006-05-26 |
| FR2841333A1 (en) | 2003-12-26 |
| EP1375345A1 (en) | 2004-01-02 |
| EP1375345B1 (en) | 2006-06-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8332 | No legal effect for de |