NO822396L - Rakett-fartoey - Google Patents

Rakett-fartoey

Info

Publication number
NO822396L
NO822396L NO822396A NO822396A NO822396L NO 822396 L NO822396 L NO 822396L NO 822396 A NO822396 A NO 822396A NO 822396 A NO822396 A NO 822396A NO 822396 L NO822396 L NO 822396L
Authority
NO
Norway
Prior art keywords
flaps
rocket
nozzle
control
outflow
Prior art date
Application number
NO822396A
Other languages
English (en)
Norwegian (no)
Inventor
Arnold Leith Deans
Alan John Smith
Malcolm John Crozier
Original Assignee
Commw Of Australia
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 Commw Of Australia filed Critical Commw Of Australia
Publication of NO822396L publication Critical patent/NO822396L/no

Links

Classifications

    • 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
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor 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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Transmission Devices (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Toys (AREA)
  • Lubricants (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Lighting Device Outwards From Vehicle And Optical Signal (AREA)
NO822396A 1980-11-14 1982-07-09 Rakett-fartoey NO822396L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AUPE650180 1980-11-14

Publications (1)

Publication Number Publication Date
NO822396L true NO822396L (no) 1982-07-09

Family

ID=3768828

Family Applications (1)

Application Number Title Priority Date Filing Date
NO822396A NO822396L (no) 1980-11-14 1982-07-09 Rakett-fartoey

Country Status (14)

Country Link
US (1) US4562980A (fr)
EP (1) EP0065529B1 (fr)
JP (1) JPS6130143B2 (fr)
KR (1) KR870000134B1 (fr)
AU (1) AU545865B2 (fr)
BE (1) BE891122A (fr)
CA (1) CA1179192A (fr)
DE (1) DE3176208D1 (fr)
DK (1) DK154794C (fr)
ES (2) ES507134A0 (fr)
IT (1) IT1145736B (fr)
NO (1) NO822396L (fr)
NZ (1) NZ198917A (fr)
WO (1) WO1982001745A1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4949918A (en) * 1989-08-02 1990-08-21 Arszman Jerrold H Moment control of rockets
US5076511A (en) * 1990-12-19 1991-12-31 Honeywell Inc. Discrete impulse spinning-body hard-kill (disk)
US5320304A (en) * 1991-03-15 1994-06-14 The United States Of America As Represented By The Secretary Of The Navy Integrated aerodynamic fin and stowable TVC vane system
US5511745A (en) * 1994-12-30 1996-04-30 Thiokol Corporation Vectorable nozzle having jet vanes
US5806791A (en) * 1995-05-26 1998-09-15 Raytheon Company Missile jet vane control system and method
US5513084A (en) * 1995-07-10 1996-04-30 Simpson; Ted L. Holiday lighting decoration and method
US6450443B1 (en) * 2000-08-17 2002-09-17 The United States Of America As Represented By The Secretary Of The Navy High torque 2.75-inch rocket nozzle
US6754566B2 (en) * 2002-06-26 2004-06-22 The Boeing Company System and method allowing for an integrated flight loads balancing process
NO318772B1 (no) * 2003-09-24 2005-05-02 Nammo Raufoss As Rakettmotor med styrevinger i motorens dyse
FR2870932B1 (fr) * 2004-05-27 2006-08-11 Mbda France Sa Engin volant pour l'observation du sol
KR100625852B1 (ko) * 2004-10-07 2006-09-20 한국항공우주연구원 발사체의 고체모터 가동노즐 추력벡터제어용구동장치시스템의 보상제어방법 및 그 보상제어회로부
FR2946741B1 (fr) * 2009-06-12 2015-09-18 Mbda France Systeme pour le controle de la trajectoire d'un mobile mu par reaction.
US8803052B2 (en) 2010-04-08 2014-08-12 Bae Systems Information And Electronic Systems Integration Inc. Predictive roll capture
FR2967766B1 (fr) * 2010-11-24 2012-12-28 Mbda France Systeme pour piloter autour de ses axes de rotation un mobile mu par reaction, en particulier un missile
CN115325889B (zh) * 2022-09-01 2023-09-29 北京中科宇航技术有限公司 一种叶面旋转栅格舵控制系统
US11879416B1 (en) * 2022-09-09 2024-01-23 Raytheon Company Method for reducing jet tab exposure during thrust vectoring

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969017A (en) * 1948-03-19 1961-01-24 Richard B Kershner Stabilizers for jet-propelled vehicles
US2694898A (en) * 1948-08-09 1954-11-23 France Etat Device for deflecting a high-speed jet of gas ejected through a nozzle
US2919544A (en) * 1956-01-10 1960-01-05 Jr E Quimby Smith Steering mechanism for jet propelled craft
US2850977A (en) * 1956-03-13 1958-09-09 Richard J Pollak Self energized stabilizing control
US3139033A (en) * 1959-07-23 1964-06-30 Ernst D Geissler Aerodynamically stable missile
US3096049A (en) * 1960-01-25 1963-07-02 Edward S Karasinski Steering means for space vehicles missiles and high altitude flying craft
US3246468A (en) * 1962-08-10 1966-04-19 Thiokol Chemical Corp Steering means for rockets
DE1199663B (de) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Duese fuer Raketen oder raketenartige Geschosse
US3260205A (en) * 1964-09-28 1966-07-12 Aerojet General Co Fin actuated spin vane control device and method
US3369772A (en) * 1964-10-08 1968-02-20 Honeywell Inc Control apparatus
DE1298912B (de) * 1965-12-10 1969-07-03 Messerschmitt Boelkow Blohm Schubvektorsteuerung fuer einen raketengetriebenen Flugkoerper mit mindestens einem Strahlablenker
GB1230760A (fr) * 1967-04-28 1971-05-05
NO130026B (fr) * 1969-08-12 1974-06-24 Imp Metal Ind Kynoch Ltd
US3786993A (en) * 1972-05-22 1974-01-22 Imp Metal Ind Kynoch Ltd Control systems for rocket motors
US3743184A (en) * 1972-07-07 1973-07-03 Us Navy Cylindrical throat nozzle with movable sonic blades for obtaining dual area throat and thrust vector control
US3926390A (en) * 1972-11-21 1975-12-16 Us Army Control valve logic
US3986683A (en) * 1974-03-27 1976-10-19 The United States Of America As Represented By The Secretary Of The Air Force Jet tab steerable missile
US4023749A (en) * 1975-12-08 1977-05-17 The United States Of America As Represented By The Secretary Of The Army Directional control system for artillery missiles
SE408323B (sv) * 1976-06-08 1979-06-05 Bofors Ab Styranordning for en ballistisk enhet
DE2649672C3 (de) * 1976-10-29 1979-10-11 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Ablenkvorrichtung für Düsenstrahlen
US4131246A (en) * 1977-02-04 1978-12-26 Textron Inc. Thrust vector control actuation system
US4272040A (en) * 1978-07-14 1981-06-09 General Dynamics, Pomona Division Aerodynamic control mechanism for thrust vector control
US4274610A (en) * 1978-07-14 1981-06-23 General Dynamics, Pomona Division Jet tab control mechanism for thrust vector control
US4432512A (en) * 1978-08-31 1984-02-21 British Aerospace Public Limited Company Jet propulsion efflux outlets

Also Published As

Publication number Publication date
DE3176208D1 (en) 1987-06-25
KR830007363A (ko) 1983-10-19
DK308382A (da) 1982-07-09
ES8302198A1 (es) 1982-12-16
ES8207277A1 (es) 1982-09-01
US4562980A (en) 1986-01-07
EP0065529B1 (fr) 1987-05-20
IT8168488A0 (it) 1981-11-16
ES509190A0 (es) 1982-12-16
ES507134A0 (es) 1982-09-01
WO1982001745A1 (fr) 1982-05-27
KR870000134B1 (ko) 1987-02-12
NZ198917A (en) 1985-01-31
CA1179192A (fr) 1984-12-11
EP0065529A4 (fr) 1984-11-16
BE891122A (fr) 1982-03-01
IT1145736B (it) 1986-11-05
DK154794C (da) 1989-06-12
JPS57501874A (fr) 1982-10-21
DK154794B (da) 1988-12-19
EP0065529A1 (fr) 1982-12-01
JPS6130143B2 (fr) 1986-07-11
AU7727481A (en) 1982-06-07
AU545865B2 (en) 1985-08-01

Similar Documents

Publication Publication Date Title
NO822396L (no) Rakett-fartoey
US2850977A (en) Self energized stabilizing control
US4759514A (en) Tail rotor yaw position control for a helicopter
US3116040A (en) Supersonic rotary wing platform
ES2349731T3 (es) Sistemas y métodos de control de vuelo mejorado para una aeronave a reacción de triple modo.
JP3320828B2 (ja) ヘリコプタ、および単一の主回転翼により作用されるトルクに対向する方法
US5799901A (en) Rotor blade swashplate-axis rotation and gyroscopic moments compensator
GB2030098A (en) A composite aircraft
US3946968A (en) Apparatus and method for aerodynamic cross-coupling reduction
CN103625642A (zh) 一种控制混合式直升机襟翼和水平尾翼的方法
EP0747655A2 (fr) Pilote automatique de type multiple pour missile
US12122516B2 (en) Thrust unit for a propulsion device and associated propulsion device
JP3501871B2 (ja) 輸送機
RU2392186C2 (ru) Способ управления двухдвигательным самолетом и система для его осуществления
RU94029351A (ru) Космический аппарат для спуска в атмосфере планеты и способ спуска космического аппарата в атмосфере планеты
NO145053B (no) Fremgangsmaate til styring av et helikopter, og apparat til utfoerelse av fremgangsmaaten
US2941600A (en) Helicopter propulsion system
US4140290A (en) V/STOL aircraft with thrust control
US2915261A (en) Aerodyne with wings having variable sweep-back
US3070330A (en) Attitude and propellant flow control system and method
RU2043954C1 (ru) Способ спуска ускорителя ракеты космического назначения в посадочную зону и устройство для его осуществления
US2620150A (en) Airplane control
US11292589B2 (en) Method of automatically adjusting lift provided for a hybrid rotorcraft, and an associated hybrid rotorcraft
US5080301A (en) Glide Missile
US12371155B2 (en) Coupling method for redundant servo devices of an actuator control system, associated system and device