FR2058224A1 - - Google Patents

Info

Publication number
FR2058224A1
FR2058224A1 FR7029584A FR7029584A FR2058224A1 FR 2058224 A1 FR2058224 A1 FR 2058224A1 FR 7029584 A FR7029584 A FR 7029584A FR 7029584 A FR7029584 A FR 7029584A FR 2058224 A1 FR2058224 A1 FR 2058224A1
Authority
FR
France
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.)
Granted
Application number
FR7029584A
Other languages
French (fr)
Other versions
FR2058224B1 (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.)
Imperial Metal Industries Kynoch Ltd
Imperial Metal Industries Ltd
Original Assignee
Imperial Metal Industries Kynoch Ltd
Imperial Metal Industries Ltd
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 Imperial Metal Industries Kynoch Ltd, Imperial Metal Industries Ltd filed Critical Imperial Metal Industries Kynoch Ltd
Publication of FR2058224A1 publication Critical patent/FR2058224A1/fr
Application granted granted Critical
Publication of FR2058224B1 publication Critical patent/FR2058224B1/fr
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
    • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Testing Of Engines (AREA)
  • Cleaning In General (AREA)
  • Toys (AREA)
  • Manufacture And Refinement Of Metals (AREA)
FR7029584A 1969-08-12 1970-08-11 Expired FR2058224B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB4031369 1969-08-12
GB5739569 1969-11-24

Publications (2)

Publication Number Publication Date
FR2058224A1 true FR2058224A1 (en) 1971-05-28
FR2058224B1 FR2058224B1 (en) 1973-08-10

Family

ID=26264370

Family Applications (2)

Application Number Title Priority Date Filing Date
FR7029583A Expired FR2058223B1 (en) 1969-08-12 1970-08-11
FR7029584A Expired FR2058224B1 (en) 1969-08-12 1970-08-11

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR7029583A Expired FR2058223B1 (en) 1969-08-12 1970-08-11

Country Status (6)

Country Link
JP (1) JPS5012839B1 (en)
CH (2) CH516738A (en)
DE (2) DE2040135C3 (en)
FR (2) FR2058223B1 (en)
NO (1) NO130026B (en)
SE (1) SE375954B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ198917A (en) * 1980-11-14 1985-01-31 Commw Of Australia Rocket controlled by spoiler tabs in exhaust
US7155898B2 (en) * 2004-04-13 2007-01-02 Aerojet-General Corporation Thrust vector control system for a plug nozzle rocket engine
WO2015125766A1 (en) * 2014-02-19 2015-08-27 三菱重工業株式会社 Thrust vectoring device
JP6361404B2 (en) * 2014-09-17 2018-07-25 三菱重工業株式会社 Thrust deflector and flying object equipped with thrust deflector
JP6361456B2 (en) * 2014-10-17 2018-07-25 三菱重工業株式会社 Thrust deflecting device, thrust deflecting method, and flying object
CN112682215B (en) * 2020-12-23 2022-04-19 武汉量宇智能科技有限公司 Small-bore spoiler formula thrust vector control mechanism

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3245620A (en) * 1961-12-13 1966-04-12 Gen Motors Corp Missile steering control
US3384325A (en) * 1965-12-10 1968-05-21 Bolkow Gmbh Missile with thrust vector control

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2694989A (en) * 1950-01-06 1954-11-23 Directie Staatsmijnen Nl Apparatus for the automatic firing of solid fuel such as coke and similar fuels, and in particular relating to the firing of large coke
BE502140A (en) * 1950-03-29
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
US3150486A (en) * 1963-03-08 1964-09-29 Heinrich J Hollstein Cooled reaction control device
FR1416222A (en) * 1963-04-03 1965-10-29 British Aircraft Corp Ltd Improvements to jet propulsion engines
FR1458137A (en) * 1965-03-16 1966-03-04 Nord Aviation Method and device for guiding an aerodyne

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3245620A (en) * 1961-12-13 1966-04-12 Gen Motors Corp Missile steering control
US3384325A (en) * 1965-12-10 1968-05-21 Bolkow Gmbh Missile with thrust vector control

Also Published As

Publication number Publication date
DE2040134C3 (en) 1978-07-20
DE2040135A1 (en) 1971-02-25
JPS5012839B1 (en) 1975-05-15
FR2058224B1 (en) 1973-08-10
DE2040134B2 (en) 1977-11-24
CH516738A (en) 1971-12-15
FR2058223B1 (en) 1973-08-10
DE2040135B2 (en) 1978-01-12
NO130026B (en) 1974-06-24
SE375954B (en) 1975-05-05
DE2040134A1 (en) 1971-02-25
DE2040135C3 (en) 1982-10-07
FR2058223A1 (en) 1971-05-28
CH514781A (en) 1971-10-31

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