GB1225435A - - Google Patents

Info

Publication number
GB1225435A
GB1225435A GB1225435DA GB1225435A GB 1225435 A GB1225435 A GB 1225435A GB 1225435D A GB1225435D A GB 1225435DA GB 1225435 A GB1225435 A GB 1225435A
Authority
GB
United Kingdom
Prior art keywords
jet
acceleration
crusing
intercepted
deflected
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
Other languages
English (en)
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 filed Critical
Publication of GB1225435A publication Critical patent/GB1225435A/en
Expired legal-status Critical Current

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
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
GB1225435D 1967-05-10 1968-05-10 Expired GB1225435A (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR105981 1967-05-10

Publications (1)

Publication Number Publication Date
GB1225435A true GB1225435A (enExample) 1971-03-17

Family

ID=8630620

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1225435D Expired GB1225435A (enExample) 1967-05-10 1968-05-10

Country Status (3)

Country Link
DE (1) DE1756347B1 (enExample)
FR (1) FR1602885A (enExample)
GB (1) GB1225435A (enExample)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2649672C3 (de) * 1976-10-29 1979-10-11 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Ablenkvorrichtung für Düsenstrahlen

Also Published As

Publication number Publication date
DE1756347B1 (de) 1971-12-16
FR1602885A (enExample) 1971-02-08

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Legal Events

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