BE595366A - Tuyère pivotante pour fusée à combustible solide. - Google Patents

Tuyère pivotante pour fusée à combustible solide.

Info

Publication number
BE595366A
BE595366A BE595366A BE595366A BE595366A BE 595366 A BE595366 A BE 595366A BE 595366 A BE595366 A BE 595366A BE 595366 A BE595366 A BE 595366A BE 595366 A BE595366 A BE 595366A
Authority
BE
Belgium
Prior art keywords
solid fuel
swivel nozzle
fuel rocket
rocket
swivel
Prior art date
Application number
BE595366A
Other languages
English (en)
Inventor
Walter A Ledwith
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of BE595366A publication Critical patent/BE595366A/fr

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
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable 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
    • 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
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Clamps And Clips (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Testing Of Engines (AREA)
BE595366A 1960-01-04 1960-09-23 Tuyère pivotante pour fusée à combustible solide. BE595366A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US299A US3048010A (en) 1960-01-04 1960-01-04 Swiveling nozzle for solid rocket

Publications (1)

Publication Number Publication Date
BE595366A true BE595366A (fr) 1961-01-20

Family

ID=21690872

Family Applications (1)

Application Number Title Priority Date Filing Date
BE595366A BE595366A (fr) 1960-01-04 1960-09-23 Tuyère pivotante pour fusée à combustible solide.

Country Status (4)

Country Link
US (1) US3048010A (fr)
BE (1) BE595366A (fr)
CH (1) CH379967A (fr)
GB (1) GB907741A (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3230708A (en) * 1961-10-27 1966-01-25 Thiokol Chemical Corp Steerable rocket motor with gimballed nozzle means and cooling means
US3233834A (en) * 1962-07-09 1966-02-08 Aerojet General Co Sealing means for rocket nozzle and jet deflection device mounted thereon
US3251553A (en) * 1962-08-08 1966-05-17 United Aircraft Corp Pressurized nozzle gimbal
US3280563A (en) * 1962-10-26 1966-10-25 Charles F Bowersett Thrust vectoring system
US3208215A (en) * 1964-09-04 1965-09-28 Richard L Brown Gimbaled, partially submerged rocket nozzle
US3270505A (en) * 1964-10-21 1966-09-06 Norman L Crabill Control system for rocket vehicles
GB1105817A (en) * 1965-10-22 1968-03-13 Rolls Royce Jet nozzles for jet propulsion plant
US3401887A (en) * 1966-05-02 1968-09-17 Thiokol Chemical Corp Controllable rocket nozzle with pressure amplifier for reducing actuating force
GB1291586A (en) * 1969-10-23 1972-10-04 Rolls Royce Propulsive jet nozzle assembly
US3957207A (en) * 1974-08-05 1976-05-18 Chronic Bill M Gimball nozzle-trim

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB697721A (en) * 1949-01-11 1953-09-30 Fairey Aviat Co Ltd Improvements in or relating to flying bodies
US2693371A (en) * 1952-06-16 1954-11-02 Solar Aircraft Co Short flexible coupling

Also Published As

Publication number Publication date
US3048010A (en) 1962-08-07
CH379967A (de) 1964-07-15
GB907741A (en) 1962-10-10

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