CH514781A - Schubvektorsteuereinrichtung an einem Raketenmotor - Google Patents

Schubvektorsteuereinrichtung an einem Raketenmotor

Info

Publication number
CH514781A
CH514781A CH1209970A CH1209970A CH514781A CH 514781 A CH514781 A CH 514781A CH 1209970 A CH1209970 A CH 1209970A CH 1209970 A CH1209970 A CH 1209970A CH 514781 A CH514781 A CH 514781A
Authority
CH
Switzerland
Prior art keywords
rocket motor
thrust vector
vector controller
controller
thrust
Prior art date
Application number
CH1209970A
Other languages
German (de)
English (en)
Inventor
Burgess Brian
Philip Thorp Geoffrey
Original Assignee
Imp Metal Ind Kynoch Ltd Kynoc
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 Imp Metal Ind Kynoch Ltd Kynoc filed Critical Imp Metal Ind Kynoch Ltd Kynoc
Publication of CH514781A publication Critical patent/CH514781A/de

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)
  • Manufacture And Refinement Of Metals (AREA)
  • Toys (AREA)
CH1209970A 1969-08-12 1970-08-12 Schubvektorsteuereinrichtung an einem Raketenmotor CH514781A (de)

Applications Claiming Priority (2)

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

Publications (1)

Publication Number Publication Date
CH514781A true CH514781A (de) 1971-10-31

Family

ID=26264370

Family Applications (2)

Application Number Title Priority Date Filing Date
CH1209970A CH514781A (de) 1969-08-12 1970-08-12 Schubvektorsteuereinrichtung an einem Raketenmotor
CH1210270A CH516738A (de) 1969-08-12 1970-08-12 Schubvektorsteuereinrichtung an einem Raketenmotor

Family Applications After (1)

Application Number Title Priority Date Filing Date
CH1210270A CH516738A (de) 1969-08-12 1970-08-12 Schubvektorsteuereinrichtung an einem Raketenmotor

Country Status (6)

Country Link
JP (1) JPS5012839B1 (ja)
CH (2) CH514781A (ja)
DE (2) DE2040135C3 (ja)
FR (2) FR2058224B1 (ja)
NO (1) NO130026B (ja)
SE (1) SE375954B (ja)

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
US20160326987A1 (en) * 2014-02-19 2016-11-10 Mitsubishi Heavy Industries, Ltd. Thrust vectoring device
JP6361404B2 (ja) * 2014-09-17 2018-07-25 三菱重工業株式会社 推力偏向装置、および、推力偏向装置を備える飛しょう体
JP6361456B2 (ja) * 2014-10-17 2018-07-25 三菱重工業株式会社 推力偏向装置、推力偏向方法、及び飛しょう体
CN112682215B (zh) * 2020-12-23 2022-04-19 武汉量宇智能科技有限公司 小口径扰流片式推力矢量控制机构

Family Cites Families (8)

* 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 (ja) * 1950-03-29
US3020714A (en) * 1956-07-03 1962-02-13 Snecma Device for controlling the jet of a reaction propulsion motor
US3245620A (en) * 1961-12-13 1966-04-12 Gen Motors Corp Missile steering control
US3150486A (en) * 1963-03-08 1964-09-29 Heinrich J Hollstein Cooled reaction control device
FR1416222A (fr) * 1963-04-03 1965-10-29 British Aircraft Corp Ltd Perfectionnements apportés aux moteurs à propulsion par réaction
FR1458137A (fr) * 1965-03-16 1966-03-04 Nord Aviation Procédé et dispositif de guidage d'un aérodyne
DE1298912B (de) * 1965-12-10 1969-07-03 Messerschmitt Boelkow Blohm Schubvektorsteuerung fuer einen raketengetriebenen Flugkoerper mit mindestens einem Strahlablenker

Also Published As

Publication number Publication date
SE375954B (ja) 1975-05-05
DE2040134A1 (de) 1971-02-25
DE2040134B2 (de) 1977-11-24
FR2058223A1 (ja) 1971-05-28
FR2058223B1 (ja) 1973-08-10
DE2040135B2 (de) 1978-01-12
CH516738A (de) 1971-12-15
DE2040135A1 (de) 1971-02-25
JPS5012839B1 (ja) 1975-05-15
NO130026B (ja) 1974-06-24
FR2058224B1 (ja) 1973-08-10
FR2058224A1 (ja) 1971-05-28
DE2040134C3 (de) 1978-07-20
DE2040135C3 (de) 1982-10-07

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Legal Events

Date Code Title Description
PL Patent ceased