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GB2068311B - Jet reaction propelled flying body - Google Patents

Jet reaction propelled flying body

Info

Publication number
GB2068311B
GB2068311B GB8041067A GB8041067A GB2068311B GB 2068311 B GB2068311 B GB 2068311B GB 8041067 A GB8041067 A GB 8041067A GB 8041067 A GB8041067 A GB 8041067A GB 2068311 B GB2068311 B GB 2068311B
Authority
GB
United Kingdom
Prior art keywords
flying body
jet reaction
propelled flying
reaction propelled
jet
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB8041067A
Other languages
English (en)
Other versions
GB2068311A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dornier GmbH
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 GB2068311A publication Critical patent/GB2068311A/en
Application granted granted Critical
Publication of GB2068311B publication Critical patent/GB2068311B/en
Expired legal-status Critical Current

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)
GB8041067A 1980-01-30 1980-12-22 Jet reaction propelled flying body Expired GB2068311B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3003231A DE3003231C2 (de) 1980-01-30 1980-01-30 Steuereinrichtung für durch Strahlreaktion angetriebene Flugkörper, Raketen o.dgl.

Publications (2)

Publication Number Publication Date
GB2068311A GB2068311A (en) 1981-08-12
GB2068311B true GB2068311B (en) 1984-02-15

Family

ID=6093235

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8041067A Expired GB2068311B (en) 1980-01-30 1980-12-22 Jet reaction propelled flying body

Country Status (5)

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

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 (ru) * 1998-03-20 1998-12-10 Акционерное общество открытого типа "ОКБ Сухого" Система управления двухдвигательного самолета посредством управления вектором тяги
RU2122511C1 (ru) * 1998-06-22 1998-11-27 Акционерное общество открытого типа "ОКБ Сухого" Управление самолетом посредством управления вектором тяги
DE102008022289B4 (de) 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper
JP5123964B2 (ja) 2010-02-26 2013-01-23 三菱重工業株式会社 航空機の制御システム、航空機の制御方法、及び航空機
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
SE8100747L (sv) 1981-07-31
GB2068311A (en) 1981-08-12
DE3003231A1 (de) 1981-08-06
IT1167303B (it) 1987-05-13
DE3003231C2 (de) 1984-01-05
IT8068752A0 (it) 1980-11-14
FR2474439A1 (fr) 1981-07-31

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee