DE3242392A1 - Device which allows aircraft to deflect rockets which are operated against them - Google Patents
Device which allows aircraft to deflect rockets which are operated against themInfo
- Publication number
- DE3242392A1 DE3242392A1 DE19823242392 DE3242392A DE3242392A1 DE 3242392 A1 DE3242392 A1 DE 3242392A1 DE 19823242392 DE19823242392 DE 19823242392 DE 3242392 A DE3242392 A DE 3242392A DE 3242392 A1 DE3242392 A1 DE 3242392A1
- Authority
- DE
- Germany
- Prior art keywords
- rockets
- deflect
- aircraft
- operated against
- allows aircraft
- 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- Withdrawn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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/14—Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Retarders (AREA)
Abstract
Description
Benennung: Einrichtung, die es flugzeugen ermöglicht, den gegenDesignation: device that enables aircraft to attack
sie eingesetzten Raketen auszuweichen Militärflugzeuge, die sich im knflug auf ihr Einsatzziel befinden, sind hauptsächlich durch Raketen bedroht. Um diesen zu entgehen sollen nach der hiermit angemeldeten Idee am oder im Flugzeugrumpf, oder an Tragflächen Triebwerke angebracht werden, deren Schub quer zur Flugrichtung wirkt. Durch kurzzeitige Zündung dieser Triebwerke erfolgt ein Schub der das Flugzeug so plötzlich seitwärts verschiebt daß die gegen dasselbe eingesetzten Raketen trotz ihrer Such- und Lenkvorrichtung diesem Ausweichmanöver nicht folgen können, weil sie dazu viel zu enge Kurven fliegen müssen, was bei ihrer Gesenwindigkeit nicht möglich ist. Die Zündung dieser Triebwerke erfolgt entweder jedesmal durch den Piloten oder mittels Binschalten eines Programms, welches im Kampfgebiet dem Flugzeug einen Zickzackkurs ermöglicht1 they deployed missiles to dodge military aircraft that are themselves are approaching their target are threatened mainly by missiles. In order to avoid this, according to the hereby registered idea on or in the aircraft fuselage, or engines are attached to wings, the thrust of which is transverse to the direction of flight works. Brief ignition of these engines causes the aircraft to thrust so suddenly shifted sideways that the missiles deployed against it in spite of it their search and steering device cannot follow this evasive maneuver because To do this, they have to fly much too tight turns, which is not the case with their speed is possible. The ignition of these engines is done either by the pilot each time or by connecting a program, which the aircraft in the combat area Zigzag course enables 1
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19823242392 DE3242392A1 (en) | 1982-11-16 | 1982-11-16 | Device which allows aircraft to deflect rockets which are operated against them |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19823242392 DE3242392A1 (en) | 1982-11-16 | 1982-11-16 | Device which allows aircraft to deflect rockets which are operated against them |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3242392A1 true DE3242392A1 (en) | 1984-05-17 |
Family
ID=6178282
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19823242392 Withdrawn DE3242392A1 (en) | 1982-11-16 | 1982-11-16 | Device which allows aircraft to deflect rockets which are operated against them |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3242392A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002102660A1 (en) * | 2001-06-20 | 2002-12-27 | Tom Kusic | Aircraft spiralling mechanism |
US7635104B1 (en) | 2001-06-22 | 2009-12-22 | Tom Kusic | Aircraft spiraling mechanism with jet assistance—B |
US7637453B2 (en) | 2001-06-22 | 2009-12-29 | Tom Kusic | Aircraft spiraling mechanism with jet assistance - A |
US7642491B2 (en) | 2007-03-19 | 2010-01-05 | Tom Kusic | Aircraft spiraling mechanism with jet assistance—D |
-
1982
- 1982-11-16 DE DE19823242392 patent/DE3242392A1/en not_active Withdrawn
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002102660A1 (en) * | 2001-06-20 | 2002-12-27 | Tom Kusic | Aircraft spiralling mechanism |
US7635104B1 (en) | 2001-06-22 | 2009-12-22 | Tom Kusic | Aircraft spiraling mechanism with jet assistance—B |
US7637453B2 (en) | 2001-06-22 | 2009-12-29 | Tom Kusic | Aircraft spiraling mechanism with jet assistance - A |
US7825359B2 (en) | 2006-11-20 | 2010-11-02 | Tom Kusic | Aircraft spiraling mechanism with jet assistance - E |
US7642491B2 (en) | 2007-03-19 | 2010-01-05 | Tom Kusic | Aircraft spiraling mechanism with jet assistance—D |
US7800033B1 (en) | 2007-03-19 | 2010-09-21 | Tom Kusic | Separation activated missile spiraling mechanism—FA |
US7812294B2 (en) | 2007-03-19 | 2010-10-12 | Tom Kusic | Aircraft spiraling mechanism with jet assistance-f |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8139 | Disposal/non-payment of the annual fee |