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SE8100747L - CONTROL FOR RADIATED AIRCRAFT AIRCRAFT, ROCKETS AND LIKE - Google Patents

CONTROL FOR RADIATED AIRCRAFT AIRCRAFT, ROCKETS AND LIKE

Info

Publication number
SE8100747L
SE8100747L SE8100747A SE8100747A SE8100747L SE 8100747 L SE8100747 L SE 8100747L SE 8100747 A SE8100747 A SE 8100747A SE 8100747 A SE8100747 A SE 8100747A SE 8100747 L SE8100747 L SE 8100747L
Authority
SE
Sweden
Prior art keywords
aircraft
control
rockets
radiated
nozzles
Prior art date
Application number
SE8100747A
Other languages
Unknown language ( )
Swedish (sv)
Inventor
R Idiens
Original Assignee
Dornier Gmbh
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 Dornier Gmbh filed Critical Dornier Gmbh
Publication of SE8100747L publication Critical patent/SE8100747L/en

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
    • F42B10/60—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)
  • 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)
  • Nozzles (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

For improved control of motion about its pitching or yaw axis, a flying body has two or more nozzles (10, 12) with their axes (X%, X%) on a circle concentric with the longitudinal axis (X) of the body and convergent and inclined to the longitudinal axis at equal angles (a). A rotatable spoiler plate (18), (Fig. 3, not shown) with holes may be arranged behind the nozzles, so that the plate can interrupt and deflect the propellant gas jets to generate rolling control moments. <IMAGE>
SE8100747A 1980-01-30 1981-01-30 CONTROL FOR RADIATED AIRCRAFT AIRCRAFT, ROCKETS AND LIKE SE8100747L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3003231A DE3003231C2 (en) 1980-01-30 1980-01-30 Control device for missiles, rockets or the like driven by beam reaction.

Publications (1)

Publication Number Publication Date
SE8100747L true SE8100747L (en) 1981-07-31

Family

ID=6093235

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8100747A SE8100747L (en) 1980-01-30 1981-01-30 CONTROL FOR RADIATED AIRCRAFT AIRCRAFT, ROCKETS AND LIKE

Country Status (5)

Country Link
DE (1) DE3003231C2 (en)
FR (1) FR2474439A1 (en)
GB (1) GB2068311B (en)
IT (1) IT1167303B (en)
SE (1) SE8100747L (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2251834B (en) * 1983-02-22 1992-12-16 George Alexander Tarrant Guided missiles
GB2148875B (en) * 1983-10-24 1987-01-28 Standard Telephones Cables Ltd Optical fibre preform manufacture
RU2122963C1 (en) * 1998-03-20 1998-12-10 Акционерное общество открытого типа "ОКБ Сухого" System of control of twin-engined aeroplane through control of thrust vector
RU2122511C1 (en) * 1998-06-22 1998-11-27 Акционерное общество открытого типа "ОКБ Сухого" Control of aircraft by means of thrust vector control
DE102008022289B4 (en) 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. missile
JP5123964B2 (en) 2010-02-26 2013-01-23 三菱重工業株式会社 Aircraft control system, aircraft control method, and aircraft
GB201312593D0 (en) 2013-07-13 2013-08-28 Mbda Uk Ltd A thrust flow powered vehicle

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB875205A (en) * 1958-12-31 1961-08-16 Ici Ltd Improvements relating to rocket propulsion
US3057581A (en) * 1959-06-25 1962-10-09 United Aircraft Corp Rocket vectoring arrangement
US3070330A (en) * 1961-03-20 1962-12-25 William J D Escher Attitude and propellant flow control system and method
US3127740A (en) * 1962-10-17 1964-04-07 United Aircraft Corp Clustered rocket nozzles
US4254620A (en) * 1978-02-27 1981-03-10 The Boeing Company Jet engine multiduct noise suppressor

Also Published As

Publication number Publication date
GB2068311A (en) 1981-08-12
DE3003231A1 (en) 1981-08-06
IT1167303B (en) 1987-05-13
DE3003231C2 (en) 1984-01-05
IT8068752A0 (en) 1980-11-14
GB2068311B (en) 1984-02-15
FR2474439A1 (en) 1981-07-31

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