SE432832B - Anordning for att styra en missil under banfaserna med lag respektive hog hastighet - Google Patents

Anordning for att styra en missil under banfaserna med lag respektive hog hastighet

Info

Publication number
SE432832B
SE432832B SE7710842A SE7710842A SE432832B SE 432832 B SE432832 B SE 432832B SE 7710842 A SE7710842 A SE 7710842A SE 7710842 A SE7710842 A SE 7710842A SE 432832 B SE432832 B SE 432832B
Authority
SE
Sweden
Prior art keywords
managing
high speed
respective high
speed phase
missile during
Prior art date
Application number
SE7710842A
Other languages
English (en)
Swedish (sv)
Other versions
SE7710842L (sv
Inventor
G F East
C E Hallum
Original Assignee
Ford Aerospace & Communication
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 Ford Aerospace & Communication filed Critical Ford Aerospace & Communication
Publication of SE7710842L publication Critical patent/SE7710842L/xx
Publication of SE432832B publication Critical patent/SE432832B/xx

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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
SE7710842A 1976-10-04 1977-09-28 Anordning for att styra en missil under banfaserna med lag respektive hog hastighet SE432832B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/729,512 US4085909A (en) 1976-10-04 1976-10-04 Combined warm gas fin and reaction control servo

Publications (2)

Publication Number Publication Date
SE7710842L SE7710842L (sv) 1978-04-05
SE432832B true SE432832B (sv) 1984-04-16

Family

ID=24931391

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7710842A SE432832B (sv) 1976-10-04 1977-09-28 Anordning for att styra en missil under banfaserna med lag respektive hog hastighet

Country Status (7)

Country Link
US (1) US4085909A (de)
BE (1) BE859372A (de)
CH (1) CH627551A5 (de)
DE (1) DE2743371C2 (de)
GB (1) GB1544727A (de)
NL (1) NL185954C (de)
SE (1) SE432832B (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4560121A (en) * 1983-05-17 1985-12-24 The Garrett Corporation Stabilization of automotive vehicle
US4659036A (en) * 1983-09-26 1987-04-21 The Boeing Company Missile control surface actuator system
DE3410666C2 (de) * 1984-03-23 1986-03-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Stellantrieb
DE3441533A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Kopplungseinrichtung zwischen einem linear-stellglied und einem schwenkelement, insbesondere einem steuerruder
US4684080A (en) * 1985-06-06 1987-08-04 The Boeing Company Pressure gas supply for a missile and the like
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system
DE3632553C1 (de) * 1986-09-25 1987-12-17 Rheinmetall Gmbh Vorrichtung zur UEberdruckbegrenzung fuer innerhalb eines Geschosses angeordnete Brennkammern
US4826104A (en) * 1986-10-09 1989-05-02 British Aerospace Public Limited Company Thruster system
GB8803164D0 (en) * 1988-02-11 1988-08-24 British Aerospace Reaction control system
FR2657703B1 (fr) * 1990-01-26 1992-04-10 Thomson Brandt Armements Dispositif pour la commande d'attitude en roulis d'un projectile stabilise par empennage.
FR2659733B1 (fr) * 1990-03-14 1994-07-01 Aerospatiale Systeme pour le pilotage d'un missile au moyen de tuyeres laterales.
FR2659734B1 (fr) * 1990-03-14 1992-07-03 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux.
US6460801B1 (en) * 1993-11-18 2002-10-08 Lockheed Martin Corp. Precision guidance system for aircraft launched bombs
DE4438010A1 (de) * 1994-10-25 1996-05-02 Diehl Gmbh & Co Um seine Längsachse eine Rollbewegung ausführender Flugkörper
US6951317B2 (en) * 2002-09-03 2005-10-04 Honeywell International Inc. Vehicle, lightweight pneumatic pilot valve and related systems therefor
US20040084566A1 (en) * 2002-11-06 2004-05-06 Daniel Chasman Multi-nozzle grid missile propulsion system
US7108223B2 (en) 2002-11-07 2006-09-19 Raytheon Company Missile control system and method
US7287725B2 (en) * 2005-04-25 2007-10-30 Raytheon Company Missile control system and method
US7856806B1 (en) * 2006-11-06 2010-12-28 Raytheon Company Propulsion system with canted multinozzle grid
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
US8735788B2 (en) * 2011-02-18 2014-05-27 Raytheon Company Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
US9228815B2 (en) * 2011-07-04 2016-01-05 Omnitek Partners Llc Very low-power actuation devices
US9618305B2 (en) * 2012-04-24 2017-04-11 Omnitek Partners Llc Very low power actuation devices
US9121680B2 (en) * 2013-01-17 2015-09-01 Raytheon Company Air vehicle with control surfaces and vectored thrust
CN104696108A (zh) * 2013-12-10 2015-06-10 上海新跃仪表厂 一种利用火箭发动机高压煤油驱动的伺服机构
CN107128478B (zh) * 2017-05-23 2023-08-04 安徽中科中涣智能装备股份有限公司 一种折叠机翼的快速展开装置
CN113566658A (zh) * 2021-07-08 2021-10-29 北京星途探索科技有限公司 一种模块尾舱及舵控传动机构

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2692475A (en) * 1950-10-11 1954-10-26 Edwin H Hull Rocket steering means
DE1172156B (de) * 1959-04-23 1964-06-11 Boelkow Entwicklungen Kg Aerodynamisch lenkbarer, rueckstossgetriebener Flugkoerper
US3304029A (en) * 1963-12-20 1967-02-14 Chrysler Corp Missile directional control system
US3276376A (en) * 1964-09-30 1966-10-04 Robert W Cubbison Thrust and direction control apparatus
US3286956A (en) * 1965-07-19 1966-11-22 Douglas Aircraft Co Inc Missile control system
US3453828A (en) * 1966-03-01 1969-07-08 Plessey Co Ltd Rocket propulsion unit for operation by liquid monofuel
US3415466A (en) * 1966-05-16 1968-12-10 Chandler Evans Inc Time response matching process and product
US3430536A (en) * 1967-03-21 1969-03-04 Chandler Evans Inc Time modulated pneumatically actuated control mechanism
US3692258A (en) * 1968-10-03 1972-09-19 Arthur R Parilla Missile configurations,controls and utilization techniques
US3637167A (en) * 1969-11-05 1972-01-25 Mc Donnell Douglas Corp Missile steering system
SE377719C (sv) * 1970-04-30 1978-11-20 Hawker Siddeley Dynamics Ltd Anordning for styrning och framatdrivande av suft- eller rymdfarkost

Also Published As

Publication number Publication date
CH627551A5 (de) 1982-01-15
NL7710212A (nl) 1978-04-06
SE7710842L (sv) 1978-04-05
NL185954B (nl) 1990-03-16
GB1544727A (en) 1979-04-25
DE2743371C2 (de) 1983-01-05
US4085909A (en) 1978-04-25
DE2743371A1 (de) 1978-04-13
NL185954C (nl) 1990-08-16
BE859372A (fr) 1978-02-01

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