GB2418008A - Missile interceptor - Google Patents
Missile interceptor Download PDFInfo
- Publication number
- GB2418008A GB2418008A GB0420343A GB0420343A GB2418008A GB 2418008 A GB2418008 A GB 2418008A GB 0420343 A GB0420343 A GB 0420343A GB 0420343 A GB0420343 A GB 0420343A GB 2418008 A GB2418008 A GB 2418008A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missile
- interceptor
- thrust
- missile interceptor
- exhaust
- 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.)
- Withdrawn
Links
Classifications
-
- 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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
Abstract
A missile interceptor comprises a small jet engine 8 placed inside a spherical steel ball to take in air at 5 and exhaust it as thrust in 6 and 7. Exhaust produces a vertical thrust only which keeps the missile interceptor in the air, while exhaust 6 acts as a thrust deviator and steers the missile interceptor to its target. The missile interceptor is also fitted with explosives, which is used to destroy the missile and radar to guide the interceptor to its target.
Description
24 1 8008 Missile interceptor This invention relates to intercepting a
missile fired at a fighter Aircraft. When missiles are fired at the fighter Aircraft, the pilot usually have to eject out of the aircraft as the plane gets shot down, this resuKs in the loss of the Aircraft and the pilot being captured. In some cases the pilot could get killed in such a missile attack.
To overcome this, the present invention proposes a missile interceptor which when released from the fighter aircraft runs into the path of an incoming missile fired at the aircraft and explodes destroying the missile.
The missile interceptor will make sure the fighter aircraft stays intact without any loss to the pilot or fighter aircraft.
Preferable, the missile interceptor has a small jet engine, which has two intakes, and three exhausts that form the thrust all bulk in a spherical steel ball.
Preferable, one of the exhausts produces thrust vertically while the other two produce thrust and points in different directions so as to make the missile interceptor move in various directions.
Preferable, the missile interceptor held in a bay under the fuselage or on the wings of the fighter aircrafts.
In figure 1,the missile interceptor 2 is stored in a bay under the fuselage of the fighter aircraft 1. 3 is one of the missile interceptor being released to intercept a missile 4.
Figure 2 shows the front view of the missile interceptor, 5 is the air intake to the small jet engine inside the missile interceptor made out of spherical steel ball. 6 is the thrust deviator where the thrust from the small jet engine is channelled in deferent directions so as to cause the missile interceptor move forward, climb, descend or turn towards its target. 7 also is the jet's exhaust that produces thrust but this is fixed and produces thrust in a vertical position only, this would keep the missile interceptor stationary at heights and in flight.
While figures 3 and 4 shows the missile interceptor's side view and top view respectively Figure 5 shows the inside of the missile interceptor, 8 is the small jet engine which takes in air at 5 and exhaust K producing thrust at 6 and 7. 7 produces thrust vertical only, which keeps the missile interceptor, balanced, steady and stationary in the air while 6 moves about thereby make the missile interceptor move forward, climb, descend or tum.
When the thrust deviator 6 is pointing backwards the missile interceptor moves forward. If K is pointing upwards the missile interceptor would descend and if the it is pointing downwards the missile interceptor would climb. The thrust deviator moves in such a way guided by radar moves towards its target.
The missile interceptor is also fitted with an explosive jacket that detonates the missile on impact. It also has radar to guide the missile interceptor to the missile.
Claims (2)
- Claims 1. A missile interceptor which runs into the path of an incomingmissile to a fighter aircraft and destroys the missile, the interceptor being powered by a small jet engine and steered by the engine thrust channelled to different directions
- 2. The jet engine thrust in claim 1 which is channelled to different directions causes the interceptor to move forward, climb, turn or descend towards its target.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0420343A GB2418008A (en) | 2004-09-13 | 2004-09-13 | Missile interceptor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0420343A GB2418008A (en) | 2004-09-13 | 2004-09-13 | Missile interceptor |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0420343D0 GB0420343D0 (en) | 2004-10-13 |
GB2418008A true GB2418008A (en) | 2006-03-15 |
Family
ID=33186988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0420343A Withdrawn GB2418008A (en) | 2004-09-13 | 2004-09-13 | Missile interceptor |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2418008A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007019105A1 (en) * | 2007-04-23 | 2008-10-30 | Langenhan, Thorsten | Object protection system e.g. for military encampment, has an alarm system and observation system with single breech-block weapon with interception shot/missile |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0724131A1 (en) * | 1995-01-27 | 1996-07-31 | British Aerospace Public Limited Company | Tethered missile system |
JPH1038499A (en) * | 1996-07-24 | 1998-02-13 | Ishikawajima Harima Heavy Ind Co Ltd | High-speed airframe |
WO2000029805A1 (en) * | 1998-11-13 | 2000-05-25 | Mashinostroitelnoe Konstruktorskoe Bjuro 'fakel' | Device for controlling a high-maneuverability missile |
WO2001090682A1 (en) * | 2000-05-25 | 2001-11-29 | Metal Storm Limited | Directional control of missiles |
US6771205B1 (en) * | 1977-07-28 | 2004-08-03 | Raytheon Company | Shipboard point defense system and elements therefor |
-
2004
- 2004-09-13 GB GB0420343A patent/GB2418008A/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6771205B1 (en) * | 1977-07-28 | 2004-08-03 | Raytheon Company | Shipboard point defense system and elements therefor |
EP0724131A1 (en) * | 1995-01-27 | 1996-07-31 | British Aerospace Public Limited Company | Tethered missile system |
JPH1038499A (en) * | 1996-07-24 | 1998-02-13 | Ishikawajima Harima Heavy Ind Co Ltd | High-speed airframe |
WO2000029805A1 (en) * | 1998-11-13 | 2000-05-25 | Mashinostroitelnoe Konstruktorskoe Bjuro 'fakel' | Device for controlling a high-maneuverability missile |
WO2001090682A1 (en) * | 2000-05-25 | 2001-11-29 | Metal Storm Limited | Directional control of missiles |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007019105A1 (en) * | 2007-04-23 | 2008-10-30 | Langenhan, Thorsten | Object protection system e.g. for military encampment, has an alarm system and observation system with single breech-block weapon with interception shot/missile |
Also Published As
Publication number | Publication date |
---|---|
GB0420343D0 (en) | 2004-10-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |