SU1740970A1 - Electric communication center for separable parts of missiles - Google Patents

Electric communication center for separable parts of missiles Download PDF

Info

Publication number
SU1740970A1
SU1740970A1 SU904783990A SU4783990A SU1740970A1 SU 1740970 A1 SU1740970 A1 SU 1740970A1 SU 904783990 A SU904783990 A SU 904783990A SU 4783990 A SU4783990 A SU 4783990A SU 1740970 A1 SU1740970 A1 SU 1740970A1
Authority
SU
USSR - Soviet Union
Prior art keywords
cable
missiles
parts
electric communication
knife
Prior art date
Application number
SU904783990A
Other languages
Russian (ru)
Inventor
Владислав Иванович Ягодин
Виктор Васильевич Королев
Александр Михайлович Новиков
Original Assignee
Головное конструкторское бюро Научно-производственного объединения "Энергия"
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 Головное конструкторское бюро Научно-производственного объединения "Энергия" filed Critical Головное конструкторское бюро Научно-производственного объединения "Энергия"
Priority to SU904783990A priority Critical patent/SU1740970A1/en
Application granted granted Critical
Publication of SU1740970A1 publication Critical patent/SU1740970A1/en

Links

Landscapes

  • Removal Of Insulation Or Armoring From Wires Or Cables (AREA)

Abstract

Изобретение относитс  к электроразр дным устройствам кабельной св зи раздел ющихс  блоков ракет, частей космических аппаратов и др. летательных аппаратов. Целью изобретени   вл етс  улучшение эксплуатационных характеристик путем снижени  ударных нагрузок и усилий разрыва кабел  при разделении частей летательных аппаратов. Устройство содержит кабель 1, пропущенный через уплотнительный элемент 2, и нож 3 цилиндрической формы, закрепленный на одном ракетном блоке 7; другой конец кабел  закреплен на втором ракетном блоке. В зависимости от толщины кабел  он может быть разделен на несколько жгутов различной длины 2 ил сл сThe invention relates to electric discharge cable communication devices for separating blocks of rockets, parts of spacecraft, and other aircraft. The aim of the invention is to improve the performance by reducing shock loads and cable breaking forces when separating parts of aircraft. The device contains a cable 1, passed through the sealing element 2, and a knife 3 of cylindrical shape, mounted on one rocket unit 7; the other end of the cable is attached to the second rocket unit. Depending on the cable thickness, it can be divided into several bundles of various lengths 2 or more.

Description

77

/ГЛ/ Hl

фиг. 2FIG. 2

Claims (1)

Формула изобретенияClaim Узел электрической связи разделяемых частей ракет, содержащий кабель и механический нож, отличающийся тем, что, с целью улучшения эксплуатационных характеристик путем снижения ударных нагрузок и усилий разрыва кабеля при разделении частей, в нем механический нож выполнен в виде цилиндра с острой режущей кромкой, кабель расположен внутри цилиндрического ножа и разделен на несколько отдельных жгутов различной длины, при этом между кабелем и жгутом размещено уплотнение.An electric communication unit for the separated parts of the missiles, containing a cable and a mechanical knife, characterized in that, in order to improve operational characteristics by reducing shock loads and cable breaking forces during separation of the parts, the mechanical knife is made in it in the form of a cylinder with a sharp cutting edge, the cable is located inside a cylindrical knife and is divided into several separate bundles of different lengths, while a seal is placed between the cable and the bundle. Buff А фиг. 2Buff A of FIG. 2
SU904783990A 1990-01-22 1990-01-22 Electric communication center for separable parts of missiles SU1740970A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU904783990A SU1740970A1 (en) 1990-01-22 1990-01-22 Electric communication center for separable parts of missiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU904783990A SU1740970A1 (en) 1990-01-22 1990-01-22 Electric communication center for separable parts of missiles

Publications (1)

Publication Number Publication Date
SU1740970A1 true SU1740970A1 (en) 1992-06-15

Family

ID=21492354

Family Applications (1)

Application Number Title Priority Date Filing Date
SU904783990A SU1740970A1 (en) 1990-01-22 1990-01-22 Electric communication center for separable parts of missiles

Country Status (1)

Country Link
SU (1) SU1740970A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6076467A (en) * 1997-09-26 2000-06-20 Construcciones Aeronauticas, S.A. System for attaching and separating satellites
RU2635704C1 (en) * 2016-07-28 2017-11-15 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Device for connection and disconnection of air vehicle separated stages electrical connections

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Разъемы низкочастотные Справочнику 1 М., МЭП, 1969. с. 18-21. Разработка ГКБ НПО Энерги чертеж 0510-0, 1983,прототип. *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6076467A (en) * 1997-09-26 2000-06-20 Construcciones Aeronauticas, S.A. System for attaching and separating satellites
RU2635704C1 (en) * 2016-07-28 2017-11-15 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Device for connection and disconnection of air vehicle separated stages electrical connections

Similar Documents

Publication Publication Date Title
US3461801A (en) Multi-canister ejecting device
US4106875A (en) Explosively-separated tongue and groove joint
KR880007179A (en) Indirect Firing Fastener Drive
SU1740970A1 (en) Electric communication center for separable parts of missiles
IL67724A0 (en) An improved razor blade assembly
IT8122141A0 (en) OF THE HULL OF A SHIP AND METHOD OF ASSEMBLY OF THE DEVICE MODULE FOR ITS IMPLEMENTATION.
US3674174A (en) Airborne dispenser
US3140886A (en) Coupling device
US2920532A (en) Cable cutter utilizing a hollow charge explosive
ES515720A0 (en) IMPROVEMENTS IN A TELESCOPIC WING SUPPORT STRUCTURE FOR MISSILE DEPLOYED BY SPRING.
US6148729A (en) Missile severance device
US5227579A (en) Manifold separation device
ES2016923B3 (en) EXPLOSION ENGINE THAT COMPRESSES THE MIXTURE ESPECIALLY FOR FOUR-STROKE ENGINES WITH EXTERNAL IGNITION.
SE8205501D0 (en) OUT OF CONTAINERS EXTENDABLE, BUNDLED MUNION
MX160140A (en) IMPROVEMENTS IN A METHOD TO PRESSURE WITH GAS A HERMETIC SHOCK ABSORBER, FULLY ASSEMBLED, WITHOUT INTERNAL PRESSURE
ES2094272T3 (en) DEVICE FOR THE SEPARATION OF NON-MAGNETIZABLE METALS FROM A MIX OF SOLIDS.
AU551605B2 (en) Engine oil sampling device
US3411401A (en) Explosive driven guillotine
US5698809A (en) Primer removal tool
IT8322023A0 (en) A GROOVED ELASTIC BAND. ICE PISTON ENGINE WITH
CA2230574A1 (en) Through bulkhead initiator
USD266179S (en) Arrow rest for archery bow
USD281314S (en) Junction housing for battery jumper cables
AU555526B2 (en) Aircraft engine nacelle
RU2353554C2 (en) Communication separation device