DE1677591U - TARGETING DEVICE FOR TRANSPORT MISSILES. - Google Patents

TARGETING DEVICE FOR TRANSPORT MISSILES.

Info

Publication number
DE1677591U
DE1677591U DE1954A0005136 DEA0005136U DE1677591U DE 1677591 U DE1677591 U DE 1677591U DE 1954A0005136 DE1954A0005136 DE 1954A0005136 DE A0005136 U DEA0005136 U DE A0005136U DE 1677591 U DE1677591 U DE 1677591U
Authority
DE
Germany
Prior art keywords
missiles
transport
targeting device
rocket
rod
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
Application number
DE1954A0005136
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Agurski & Walper O H G
Original Assignee
Agurski & Walper O H G
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Agurski & Walper O H G filed Critical Agurski & Walper O H G
Priority to DE1954A0005136 priority Critical patent/DE1677591U/en
Publication of DE1677591U publication Critical patent/DE1677591U/en
Expired legal-status Critical Current

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  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Description

gurski undWalper,Berlin-ZehlendorfKlopatookstr. 28 Zs el-Vorriht ranS2r ~~ ten. Die Anmeldung betrifft eine Vorridhtung die es ermöglicht, einer Rakete beim Abschuß genaue Zielrichtung zu geben. Sie ist vor allem für den Gebrauch der am 23. 1. 1954 zum Patent und (hills- weise) Gebrauchsmuster angemeldeten Vorrichtung : zum Befördern von RettunssmittelntSignaleinrichtangen usw in kleinstem, zigarren- förmigen Raketengebilde gedacht, kann aber auch zum Ablassen an- derer, entsprechend eingerichtete Raketen Verwendung finden. Die bisher in der Pyrotechnik verwendeten Raketen waren mit einem Leit-bezw. Ablaßstab versehen, der mit dem RaketenkSrper fest verbunden war und mit in die Luft getragen wurde. Während des Fluges verlagerte der Stab oft seinenSchwerpunkt, besonders wenn nicht eine genau senkrechte, sondern eine geneigte Fluglinie eingerichtet war, und brachte dadurch die Rakete aus der gewünschten Richtung. Die neue Vorrichtung sieht dagegen vor, daß die Rakete von dem Stab, der in der gewünschten Richtung eingestellt ist, abgleitet, wodurch eine exakte Flugbahn gewähreleistet ist. gurski and Walper, Berlin-Zehlendorf Klopatookstr. 28 Zs el device ranS2r ~~ ten. The application relates to a device that makes it possible to give a rocket a precise aiming point when it is launched. she is especially for the use of the patent on January 23, 1954 and (hills wise) Registered utility model device: for transporting Rescue equipment, signal devices, etc. in the smallest, cigar- shaped rocket formation, but can also be used to release of which appropriately equipped rockets are used. The rockets previously used in pyrotechnics were resp. provided with the let-off rod, which was firmly connected to the rocket body and carried in the air. During flight, the rod often shifted its center of gravity, especially when a sloping rather than a perfectly vertical line of flight was established, thereby throwing the rocket off the desired heading. The new device provides, however, that the rocket from the Stick set in the desired direction will slide, ensuring accurate trajectory.

Die Vorrichtung besteht aus einem Tragpfahl, der in der Erde befestigt wird. Ein beweglich aufgesetzter Zeiger mit schwerem Unterteil stellt sich stets senkrecht ein, auch wenn der Pfahl schräg in den Grund gesteckt werden sollte. Ein am Pfahl senkrecht ver- stellbarer Stab trägt am kurzen Arm ein gradiertes Segment ; der lange Arm ist der Ab Stab der die Flugbahn der Rakete bestimmt.The device consists of a support pole that is fixed in the ground. A movably attached pointer with a heavy base always adjusts itself vertically, even if the post is at an angle should be put into the ground. A vertically attached to the post adjustable staff carries a graduated segment on the short arm; the long arm is the ab rod that determines the missile's trajectory.

Die Rakete selbst hat einen Leitkanal, in welchen der Stab der-Vorrichtung paßt. Es können zur Erreichung der Stabilität dileh zwei Leitkanäle, gegenüberstehend, angeordnet werden. Erfindungsgemäß ist der Stab so lang, daß er über den aufgesteckten Flugkörper hinausragt, wodurch die Rakete auch noch dann gelenkt wird, wenn Fortsetzung Blatt 2 , Nau*t-ä lualpert Berl-ta vona tlio Plugboocble=Igmg otoxl* zus=o=L% hat* ja dea ZoiehnuMeti zei&t Figur 1 gan uie or in der 1) esehrotbuna tm der von 23. 141954 genamr se. a. Xa. Fig i s* Sanal . ingoagha. Mit dioaon Kann wird die R&ote auf die in, rigur 2 dargeatellte ziolv « rtohtma Dev mz&s1) 1, tzto statitpfau k tr% n da f gileaeRSeg@ 1$ si issa lotreet eis3ll'$< St< SSelRtes- ? 4 ey @ta& ia. <S<as'<EsiaMi, <m Bleht=a, D-= m =der= twzea Am vorgesehone Sio&m aesrst ss seSL ar@a As $rge@@ e&< Fiem f TrassF-'Rs. M - ja- g Ejsm Q eaon Ses AlMg'aa. g assa a fo@l<ageMm$ saSgUM. ? eag na , ä ? Ss aaetattet. « Riemgi Alsam &e in ax-SaeäaSosg geea.. sozikregeb fsis'&Ms Dst ah s@l@. t as&@e @is$llt ä&e SalTrhea 9<sM. @f a~t't'Nrd. 4< Tasihtun sah -3 aad ? @ &@r Simg .. en-,. iird, scadern die RaLote von zieh abgleitea lässtu The missile itself has a duct into which the rod of the device fits. To achieve stability, two guide channels can be arranged opposite one another. According to the invention, the rod is so long that it protrudes beyond the attached missile, which means that the missile is also steered when continued sheet 2 , Nau*t-ä lualpert Berl-ta vona tlio Plugboocble=Igmg otoxl* zus=o=L% hat* ja dea ZoiehnuMeti shows figure 1 gan uie or in the 1) esehrotbuna tm the of 23. 141954 genamr see a yes Fig is* Sanal . ingoagha. With dioaon Kann the red is set to that shown in rigur 2 ziolv « rtohtma Dev mz&s1) 1, tzto statitpfau k tr% n da f gileaeRSeg@ 1$ si issa lotreet eis3ll'$< St< SSelRtes- ? 4 hey @ta& ia. <S<as'<EsiaMi, <m Bleht=a, D-= m =der= twzea Am planned Sio&m aesrst ss seSL ar@a As $rge@@ e&< Fiem f TrassF-'Rs. M - yes- g Ejsm Q eaon Ses AlMg'aa. g assa a fo@l<ageMm$ saSgUM. ? eh well, eh? ss aaetattet. « Riemgi Alsam &e in ax-SaeäaSosg geea.. social reg fsis'&Ms Dst ah s@l@. t as&@e @is$llt ä&e SalTrhea 9<sM. @f a~t't'Nrd. 4< Tasihtun saw -3 aad ? @ &@r Simg .. en-,. iird, scad the RaLote from zug abgleitea lets u

Claims

DE1954A0005136 1954-02-09 1954-02-09 TARGETING DEVICE FOR TRANSPORT MISSILES. Expired DE1677591U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE1954A0005136 DE1677591U (en) 1954-02-09 1954-02-09 TARGETING DEVICE FOR TRANSPORT MISSILES.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1954A0005136 DE1677591U (en) 1954-02-09 1954-02-09 TARGETING DEVICE FOR TRANSPORT MISSILES.

Publications (1)

Publication Number Publication Date
DE1677591U true DE1677591U (en) 1954-06-03

Family

ID=32078469

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1954A0005136 Expired DE1677591U (en) 1954-02-09 1954-02-09 TARGETING DEVICE FOR TRANSPORT MISSILES.

Country Status (1)

Country Link
DE (1) DE1677591U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1039411B (en) * 1955-02-22 1958-09-18 Horst Walper Tow rocket and launcher
DE1072158B (en) * 1959-12-24

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1072158B (en) * 1959-12-24
DE1039411B (en) * 1955-02-22 1958-09-18 Horst Walper Tow rocket and launcher

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