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IT8068752A0 - STEERING DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSION - Google Patents

STEERING DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSION

Info

Publication number
IT8068752A0
IT8068752A0 IT8068752A IT6875280A IT8068752A0 IT 8068752 A0 IT8068752 A0 IT 8068752A0 IT 8068752 A IT8068752 A IT 8068752A IT 6875280 A IT6875280 A IT 6875280A IT 8068752 A0 IT8068752 A0 IT 8068752A0
Authority
IT
Italy
Prior art keywords
rocket
steering device
jet propulsion
similar aircraft
aircraft
Prior art date
Application number
IT8068752A
Other languages
Italian (it)
Other versions
IT1167303B (en
Inventor
Richard Idiens
Original Assignee
Dornier Gmbh
Rep Fed Di Germania
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, Rep Fed Di Germania filed Critical Dornier Gmbh
Publication of IT8068752A0 publication Critical patent/IT8068752A0/en
Application granted granted Critical
Publication of IT1167303B publication Critical patent/IT1167303B/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)
IT68752/80A 1980-01-30 1980-11-14 DIRECTION DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSION IT1167303B (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 (2)

Publication Number Publication Date
IT8068752A0 true IT8068752A0 (en) 1980-11-14
IT1167303B IT1167303B (en) 1987-05-13

Family

ID=6093235

Family Applications (1)

Application Number Title Priority Date Filing Date
IT68752/80A IT1167303B (en) 1980-01-30 1980-11-14 DIRECTION DEVICE FOR ROCKET AND SIMILAR AIRCRAFT WITH JET PROPULSION

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 (5)

* 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
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
DE3003231C2 (en) 1984-01-05
DE3003231A1 (en) 1981-08-06
IT1167303B (en) 1987-05-13
GB2068311A (en) 1981-08-12
FR2474439A1 (en) 1981-07-31
SE8100747L (en) 1981-07-31
GB2068311B (en) 1984-02-15

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