ATE329826T1 - WEAPON CONTAINING A MISSILE MOUNTED ON A STEALTH AIRCRAFT, AND WEAPON SYSTEM INCLUDING A STEALTH AIRCRAFT AND SUCH WEAPON - Google Patents
WEAPON CONTAINING A MISSILE MOUNTED ON A STEALTH AIRCRAFT, AND WEAPON SYSTEM INCLUDING A STEALTH AIRCRAFT AND SUCH WEAPONInfo
- Publication number
- ATE329826T1 ATE329826T1 AT03291082T AT03291082T ATE329826T1 AT E329826 T1 ATE329826 T1 AT E329826T1 AT 03291082 T AT03291082 T AT 03291082T AT 03291082 T AT03291082 T AT 03291082T AT E329826 T1 ATE329826 T1 AT E329826T1
- Authority
- AT
- Austria
- Prior art keywords
- weapon
- stealth aircraft
- control units
- missile
- tube
- Prior art date
Links
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 |
---|---|
ATE329826T1 true ATE329826T1 (en) | 2006-07-15 |
Family
ID=29717061
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03291082T ATE329826T1 (en) | 2002-06-20 | 2003-05-06 | WEAPON CONTAINING A MISSILE MOUNTED ON A STEALTH AIRCRAFT, AND WEAPON SYSTEM INCLUDING A STEALTH AIRCRAFT AND SUCH 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 (6)
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 |
WO2016207623A1 (en) | 2015-06-22 | 2016-12-29 | Bae Systems Plc | Aircraft payload launch system |
EP3109157A1 (en) * | 2015-06-22 | 2016-12-28 | BAE Systems PLC | Aircraft stores transport system |
JP6480024B2 (en) * | 2015-06-22 | 2019-03-06 | ビ−エイイ− システムズ パブリック リミテッド カンパニ−BAE SYSTEMS plc | Aircraft equipment transportation 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 |
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 DE DE60306038T patent/DE60306038D1/en not_active Expired - Lifetime
- 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
Also Published As
Publication number | Publication date |
---|---|
FR2841333A1 (en) | 2003-12-26 |
DE60306038D1 (en) | 2006-07-27 |
FR2841333B1 (en) | 2006-05-26 |
EP1375345A1 (en) | 2004-01-02 |
EP1375345B1 (en) | 2006-06-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU2010338161B2 (en) | System for carrying and dropping loads for a transport airplane | |
DE60010701T2 (en) | PROCEDURE FOR THE DISCONTINUANCE OF MEASURES AND DEVICE FOR STORING AND DISMISSING CONTESTED MEASURES | |
WO2006133062A3 (en) | Toy aircraft | |
ATE329826T1 (en) | WEAPON CONTAINING A MISSILE MOUNTED ON A STEALTH AIRCRAFT, AND WEAPON SYSTEM INCLUDING A STEALTH AIRCRAFT AND SUCH WEAPON | |
EP3109586A1 (en) | Projectile for intercepting a small drone | |
DE102005038382A1 (en) | Aircraft, in particular an unmanned aerial vehicle, with at least one weapon shaft | |
WO1999066418A3 (en) | Neural network controller for a pulsed rocket motor tactical missile system | |
ATE309943T1 (en) | WEAPON CONTAINING A MISSILE MOUNTED ON A STEALTH AIRCRAFT, AND WEAPON SYSTEM INCLUDING A STEALTH AIRCRAFT AND SUCH WEAPON | |
RU2008135355A (en) | CREW CABIN AND AIRPLAN CONTAINING SUCH CREW CABIN | |
EP0214166A1 (en) | Pay load projectile. | |
US6752355B1 (en) | Method and system for emergency escape from an aircraft | |
CA2429786A1 (en) | Convertible multipurpose missile launcher | |
FR2904966A3 (en) | MECHANIZED AND COMPUTER-ASSISTED BIRD-SHAPED AIRPLANE | |
DE102005042484A1 (en) | Unmanned glider aircraft comprises holding unit for bomb, and target-seeking unit | |
EP2312256A2 (en) | Missile launching device | |
IT9048566A1 (en) | IMPROVEMENT IN AIR-GROUND GUIDED MISSILES, MOUNTED ON EXTERNAL FRAMES | |
DE3803712C2 (en) | ||
WO2010074780A3 (en) | Multi-stage hyper-velocity kinetic energy missile | |
DE3906372A1 (en) | WING-STABILIZED SUBMUNITION BODY | |
DE3722038C2 (en) | ||
RU2000100556A (en) | METHOD FOR SEMI-PASSIVE SELF-GUIDING OF AIR-TO-AIR AIRCRAFT CONTROLLED ROCKET WITH A RADAR SELF-GUIDING HEAD | |
RU51724U1 (en) | UNMANNED AERIAL VEHICLE | |
WO2005036093A3 (en) | Spark-producing penetrator and method of using same | |
WO2003095304A3 (en) | Pneumatic parachute riser control | |
DE102007048073A1 (en) | Method for moving sonic buoys into a target area and missile for carrying out this method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |