UA27153C2 - Система старту і орієhтації літальhого апарата - Google Patents

Система старту і орієhтації літальhого апарата

Info

Publication number
UA27153C2
UA27153C2 UA96072972A UA96072972A UA27153C2 UA 27153 C2 UA27153 C2 UA 27153C2 UA 96072972 A UA96072972 A UA 96072972A UA 96072972 A UA96072972 A UA 96072972A UA 27153 C2 UA27153 C2 UA 27153C2
Authority
UA
Ukraine
Prior art keywords
orientation
circular body
aircraft
nozzle
profile
Prior art date
Application number
UA96072972A
Other languages
English (en)
Russian (ru)
Inventor
Іван Івановіч Архангєльській
Иван Иванович Архангельский
Євгєній Георгієвіч Болотов
Евгений Георгиевич Болотов
Владімір Сєргєєвіч Філіппов
Владимир Сергеевич Филиппов
Владімір Яковлєвіч Мізрохі
Владимир Яковлевич Мизрохи
Владімір Грігорьєвіч Свєтлов
Владимир Григорьевич Светлов
Сєргєй Грігорьєвіч Хітєнков
Сергей Григорьевич Хитенков
Віктор Леонідовіч Гайдукєвіч
Виктор Леонидович Гайдукевич
Євгєній Афанасьєвіч Шмиков
Евгений Афанасьевич Шмыков
Грігорій Андрєєвіч Станєвській
Григорий Андреевич Станевский
Original Assignee
Томсон-ЦСФ
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
Priority claimed from RU95110350A external-priority patent/RU2082946C1/ru
Application filed by Томсон-ЦСФ filed Critical Томсон-ЦСФ
Publication of UA27153C2 publication Critical patent/UA27153C2/uk

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
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
    • 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
    • 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
    • F41F3/077—Doors or covers for launching tubes
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tires In General (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

Винахід стосується систем старту й орієнтації літальних апаратів. Система включає стартові засоби, аеродинамічні рулі з приводом і засоби орієнтації, розміщені у хвостовій частині ракети й такі що включають принаймні один газогенератор і з'єднані з ним реактивні сопла. Вона обладнана кільцевим корпусом, що призначений для твердого зв'язку з корпусом літального апарата, а засоби орієнтації розміщені в кільцевому корпусі, причому внутрішня поверхня кільцевого корпуса виконана конусоподібною й покрита теплоізоляційним матеріалом з утворенням ділянки сопла, профіль якого є продовженням профілю сопла маршового двигуна ракети.
UA96072972A 1994-10-27 1995-10-27 Система старту і орієhтації літальhого апарата UA27153C2 (uk)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
RU94040077 1994-10-27
RU95110350A RU2082946C1 (ru) 1995-07-03 1995-07-03 Исполнительная система старта и ориентации ракеты
PCT/FR1995/001423 WO1996013694A1 (fr) 1994-10-27 1995-10-27 Systeme de lancement et d'orientation d'engins volants

Publications (1)

Publication Number Publication Date
UA27153C2 true UA27153C2 (uk) 2000-02-28

Family

ID=26653804

Family Applications (1)

Application Number Title Priority Date Filing Date
UA96072972A UA27153C2 (uk) 1994-10-27 1995-10-27 Система старту і орієhтації літальhого апарата

Country Status (14)

Country Link
US (1) US5823469A (uk)
EP (1) EP0737297B1 (uk)
JP (1) JP3692537B2 (uk)
KR (1) KR100404037B1 (uk)
AU (1) AU708097B2 (uk)
DE (1) DE69500842T2 (uk)
DK (1) DK0737297T3 (uk)
ES (1) ES2107921T3 (uk)
FI (1) FI111032B (uk)
IL (1) IL115749A (uk)
NO (1) NO310637B1 (uk)
TW (1) TW319825B (uk)
UA (1) UA27153C2 (uk)
WO (1) WO1996013694A1 (uk)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU183575U1 (ru) * 2018-05-18 2018-09-26 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка Летательный аппарат со стартовой двигательной установкой в транспортно-пусковом контейнере

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6584907B2 (en) 2000-03-17 2003-07-01 Ensign-Bickford Aerospace & Defense Company Ordnance firing system
US6779462B2 (en) 2001-06-04 2004-08-24 Raytheon Company Kinetic energy rod warhead with optimal penetrators
US6598534B2 (en) * 2001-06-04 2003-07-29 Raytheon Company Warhead with aligned projectiles
US7624682B2 (en) * 2001-08-23 2009-12-01 Raytheon Company Kinetic energy rod warhead with lower deployment angles
US6910423B2 (en) * 2001-08-23 2005-06-28 Raytheon Company Kinetic energy rod warhead with lower deployment angles
US7621222B2 (en) * 2001-08-23 2009-11-24 Raytheon Company Kinetic energy rod warhead with lower deployment angles
US8127686B2 (en) 2001-08-23 2012-03-06 Raytheon Company Kinetic energy rod warhead with aiming mechanism
US7624683B2 (en) 2001-08-23 2009-12-01 Raytheon Company Kinetic energy rod warhead with projectile spacing
US6931994B2 (en) * 2002-08-29 2005-08-23 Raytheon Company Tandem warhead
US7415917B2 (en) * 2002-08-29 2008-08-26 Raytheon Company Fixed deployed net for hit-to-kill vehicle
US20060021538A1 (en) * 2002-08-29 2006-02-02 Lloyd Richard M Kinetic energy rod warhead deployment system
US7017496B2 (en) 2002-08-29 2006-03-28 Raytheon Company Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators
CA2541786C (en) 2003-10-14 2008-12-30 Raytheon Company Mine counter measure system
US6920827B2 (en) * 2003-10-31 2005-07-26 Raytheon Company Vehicle-borne system and method for countering an incoming threat
US20090320711A1 (en) 2004-11-29 2009-12-31 Lloyd Richard M Munition
FR2891618B1 (fr) * 2005-10-05 2010-06-11 Giat Ind Sa Dispositif d'entrainement de gouvernes de projectile.
US8418623B2 (en) 2010-04-02 2013-04-16 Raytheon Company Multi-point time spacing kinetic energy rod warhead and system
FR2980265B1 (fr) 2011-09-21 2017-02-24 Mbda France Systeme pour le pilotage d'un engin volant a l'aide de paires de tuyeres laterales
US9372055B2 (en) * 2014-01-31 2016-06-21 The Boeing Company Passive control fin stops for air launched boosted (two stage) high speed vehicles
CN105224778A (zh) * 2014-06-09 2016-01-06 上海机电工程研究所 通用杀伤区计算方法及通用发射区计算方法
RU2563302C1 (ru) * 2014-09-03 2015-09-20 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Хвостовой блок управляемого реактивного снаряда, запускаемого из трубчатой направляющей
CN106481482B (zh) * 2015-08-26 2018-07-06 上海宇航系统工程研究所 一种小型液体发动机防热导流结构
RU2639839C1 (ru) * 2016-12-07 2017-12-22 Акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" имени И.И. Торопова" Устройство для пуска управляемого снаряда
CN108007280B (zh) * 2017-12-28 2023-08-15 北京威标至远科技发展有限公司 一种舵机防热结构
IL269920A (en) 2019-10-10 2021-04-29 Israel Aerospace Ind Ltd Missile direction
KR102125947B1 (ko) 2020-03-30 2020-06-23 정종만 용기 운반용 홀더
KR102502552B1 (ko) * 2020-12-07 2023-02-21 이병준 터빈장치

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2995319A (en) * 1958-10-09 1961-08-08 Richard B Kershner A pre-boost control device for aerial missiles
US3499364A (en) * 1959-11-19 1970-03-10 Us Navy Apparatus for submerged launching of missiles
US3084600A (en) * 1961-02-01 1963-04-09 Atlantic Res Corp Rocket launchers
US3251267A (en) * 1963-06-18 1966-05-17 Emerson Electric Co Spin rocket and launcher
US3218974A (en) * 1964-03-24 1965-11-23 Samms Adolphus Air breathing booster
US3329089A (en) * 1964-12-24 1967-07-04 Herbert L Harrison Retention-release mechanism for reaction motors and rocket interstages
US3340691A (en) * 1965-10-14 1967-09-12 Thiokol Chemical Corp Command controllable self-pressurizing liquid injection system
US3495408A (en) * 1967-11-08 1970-02-17 United Aircraft Corp Self-actuating nozzle plug
US3855789A (en) * 1968-04-05 1974-12-24 Us Navy Explosive coupling assembly
US3914935A (en) * 1969-03-17 1975-10-28 Rockwell International Corp Dual area nozzle
US3568448A (en) * 1969-04-01 1971-03-09 Thiokol Chemical Corp Ignition system for igniting a gas generator by the use of combustion gases from a solid propellant rocket motor having selective zoning capabilities
US3752425A (en) * 1970-10-28 1973-08-14 Europ Propulsion Self-propelled non-guided missiles
GB1537469A (en) * 1975-12-23 1978-12-29 Imi Kynoch Ltd Disintegrable member for controlling flow between pressure chambers
US4050351A (en) * 1976-05-04 1977-09-27 Societe Anonyme Dite: Societe Europeenne Depropulsion Assembly for launching a projectile
FR2376300A1 (fr) * 1976-12-28 1978-07-28 Luchaire Sa Dispositif pour la liaison entre deux etages d'un engin autopropulse
FR2376301A1 (fr) * 1976-12-28 1978-07-28 Luchaire Sa Engin autopropulse a etages separables
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
DE3412701C2 (de) * 1983-04-05 1997-08-21 British Aerospace Verbindungsvorrichtung
GB8324899D0 (en) * 1983-09-16 1983-10-19 Secr Defence Rocket motors
GB8417706D0 (en) * 1984-07-11 1994-01-26 British Aerospace Spin rate variation of spinning bodies
DE3686321T2 (de) * 1985-10-31 1992-12-17 British Aerospace Ausstossantrieb fuer flugkoerper.
IL79864A (en) * 1985-11-25 1994-05-30 Hughes Aircraft Co Detachable mechanism for creating a directed thrust for an aeronautical vehicle
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system
ATE106235T1 (de) * 1986-08-15 1994-06-15 Advanced Polymer Systems Inc Polymere trägerzubereitungen, herstellung und verwendung.
GB8803164D0 (en) * 1988-02-11 1988-08-24 British Aerospace Reaction control system
US4853827A (en) * 1988-08-01 1989-08-01 Rogers Corporation High dielectric multilayer capacitor
US5400713A (en) * 1994-03-09 1995-03-28 Thiokol Corporation Stage separation and thrust reduction apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU183575U1 (ru) * 2018-05-18 2018-09-26 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка Летательный аппарат со стартовой двигательной установкой в транспортно-пусковом контейнере

Also Published As

Publication number Publication date
DE69500842T2 (de) 1998-02-26
NO962653D0 (no) 1996-06-21
EP0737297B1 (fr) 1997-10-08
US5823469A (en) 1998-10-20
KR100404037B1 (ko) 2004-03-24
AU3848195A (en) 1996-05-23
JPH09507567A (ja) 1997-07-29
EP0737297A1 (fr) 1996-10-16
DE69500842D1 (de) 1997-11-13
DK0737297T3 (da) 1997-12-22
IL115749A0 (en) 1996-01-19
IL115749A (en) 2000-02-29
NO962653L (no) 1996-08-27
AU708097B2 (en) 1999-07-29
FI111032B (fi) 2003-05-15
NO310637B1 (no) 2001-07-30
ES2107921T3 (es) 1997-12-01
FI962638A0 (fi) 1996-06-26
WO1996013694A1 (fr) 1996-05-09
FI962638A (fi) 1996-08-23
TW319825B (uk) 1997-11-11
JP3692537B2 (ja) 2005-09-07

Similar Documents

Publication Publication Date Title
UA27153C2 (uk) Система старту і орієhтації літальhого апарата
US4789304A (en) Insulated propeller blade
US4650139A (en) Aerospike for attachment to space vehicle system
GB2203710B (en) Aircraft pylon
DE59001718D1 (de) Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete.
CA2324234A1 (en) Aircraft with severable body and independent passenger cabins
ES9100002A1 (es) Un avion de caza tactico de alta maniobrabilidad
GB2195108B (en) Propulsion nozzle for gas turbine engine
ES2140801T3 (es) Estatorreactor para aeronave de vuelo supersonico y/o hipersonico.
US4790499A (en) Aerospike for attachment to space vehicle system
CN101878154B (zh) 用于减小气动阻力的装置
IL139496A0 (en) Method and system for feeding a cool air inlet of the cabin of an aircraft propelled by at least one jet engine
GB2369655A (en) Hydrogen peroxide based propulsion system
US3196822A (en) Device for permitting deck landings on an aircraft-carrier in misty or foggy weather
DE3477229D1 (en) Process of intensification of the thermoenergetical cycle and air jet propulsion engines
EP1035317B1 (en) Apparatus for the Suppression of Infra Red Emissions from an Engine
US5012991A (en) Projectile with an obturator incorporating a motor
ES2013469A6 (es) Propulsor sin tobera del tipo de alargamiento reducido.
US2928237A (en) Ramjet diffuser
FR2440293A1 (fr) Dispositif de desembuage et de degivrage des vitres d'un vehicule automobile
CA2198419A1 (fr) Statoreacteur a geometrie evolutive pour aeronef
Lardellier et al. Air breathing combined engines for space transportation systems
EP0475677A1 (en) Fire retarding means for aircraft
RU95110350A (ru) Исполнительная система старта и ориентации ракеты
WEBB et al. Mach 5 turboramjet requirements and design approach