NO130026B - - Google Patents

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Info

Publication number
NO130026B
NO130026B NO302270A NO302270A NO130026B NO 130026 B NO130026 B NO 130026B NO 302270 A NO302270 A NO 302270A NO 302270 A NO302270 A NO 302270A NO 130026 B NO130026 B NO 130026B
Authority
NO
Norway
Prior art keywords
ferrous
sulfur
metal compounds
oxidation
mat
Prior art date
Application number
NO302270A
Other languages
English (en)
Norwegian (no)
Inventor
B Burgess
G Thorp
Original Assignee
Imp Metal Ind Kynoch 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 Imp Metal Ind Kynoch Ltd filed Critical Imp Metal Ind Kynoch Ltd
Publication of NO130026B publication Critical patent/NO130026B/no

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/665Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90Rocket-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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Testing Of Engines (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Toys (AREA)
  • Cleaning In General (AREA)
NO302270A 1969-08-12 1970-08-05 NO130026B (ja)

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
NO130026B true NO130026B (ja) 1974-06-24

Family

ID=26264370

Family Applications (1)

Application Number Title Priority Date Filing Date
NO302270A NO130026B (ja) 1969-08-12 1970-08-05

Country Status (6)

Country Link
JP (1) JPS5012839B1 (ja)
CH (2) CH514781A (ja)
DE (2) DE2040134C3 (ja)
FR (2) FR2058223B1 (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
DE2040135B2 (de) 1978-01-12
DE2040135C3 (de) 1982-10-07
DE2040134A1 (de) 1971-02-25
CH516738A (de) 1971-12-15
CH514781A (de) 1971-10-31
FR2058223B1 (ja) 1973-08-10
JPS5012839B1 (ja) 1975-05-15
DE2040134C3 (de) 1978-07-20
DE2040134B2 (de) 1977-11-24
SE375954B (ja) 1975-05-05
FR2058223A1 (ja) 1971-05-28
DE2040135A1 (de) 1971-02-25
FR2058224B1 (ja) 1973-08-10
FR2058224A1 (ja) 1971-05-28

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