DE1240747B - - Google Patents

Info

Publication number
DE1240747B
DE1240747B DE1963S0083648 DES0083648A DE1240747B DE 1240747 B DE1240747 B DE 1240747B DE 1963S0083648 DE1963S0083648 DE 1963S0083648 DE S0083648 A DES0083648 A DE S0083648A DE 1240747 B DE1240747 B DE 1240747B
Authority
DE
Germany
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
DE1963S0083648
Other languages
German (de)
Other versions
DE1240747C2 (de
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
Priority claimed from FR887391A external-priority patent/FR1322872A/fr
Priority claimed from FR921523A external-priority patent/FR82940E/fr
Application filed filed Critical
Application granted granted Critical
Publication of DE1240747B publication Critical patent/DE1240747B/de
Publication of DE1240747C2 publication Critical patent/DE1240747C2/de
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
    • F42B10/668—Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow
    • 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
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

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)
  • Nozzles (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
DE1963S0083648 1962-02-08 1963-02-07 Strahlschubduese fuer heisse gase mit strahlablenkung durch einfuehren eines hilfsstroemungsmittels Expired DE1240747C2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR887391A FR1322872A (fr) 1962-02-08 1962-02-08 Procédé et dispositif de déviation du jet d'une fusée
FR921523A FR82940E (fr) 1963-01-15 1963-01-15 Procédé et dispositif de déviation du jet d'une fusée

Publications (2)

Publication Number Publication Date
DE1240747B true DE1240747B (cs) 1975-07-10
DE1240747C2 DE1240747C2 (de) 1975-07-10

Family

ID=26194288

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1963S0083648 Expired DE1240747C2 (de) 1962-02-08 1963-02-07 Strahlschubduese fuer heisse gase mit strahlablenkung durch einfuehren eines hilfsstroemungsmittels

Country Status (2)

Country Link
DE (1) DE1240747C2 (cs)
GB (1) GB1028465A (cs)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2922576A1 (de) * 1979-06-02 1981-04-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Strahltriebwerk mit schubvektorsteuerung

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6336319B1 (en) * 2000-05-26 2002-01-08 General Electric Company Fluidic nozzle control system
GB2398046B (en) * 2003-01-15 2006-07-12 S & C Thermofluids Ltd The use of porous surfaces with coanda effect
GB0503874D0 (en) * 2005-02-24 2005-04-06 Rolls Royce Plc Fluid vectoring nozzle
EP1696116B1 (en) * 2005-02-24 2018-04-11 Rolls-Royce plc Thrust vectoring using fluid jets
CN104712460B (zh) * 2015-01-14 2016-04-20 北京理工大学 一种推力可控的固体火箭发动机
US11629669B1 (en) * 2019-05-31 2023-04-18 Exquadrum, Inc. Liquid monopropellant controlled solid rocket motor with aft end injection deflector

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2916873A (en) * 1958-10-22 1959-12-15 Advanced Res Associates Inc Jet deflecting apparatus

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2916873A (en) * 1958-10-22 1959-12-15 Advanced Res Associates Inc Jet deflecting apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2922576A1 (de) * 1979-06-02 1981-04-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Strahltriebwerk mit schubvektorsteuerung
US4351479A (en) * 1979-06-02 1982-09-28 Messerschmitt-Bolkow-Blohm Gmbh Jet engine with a thrust vector control

Also Published As

Publication number Publication date
DE1240747C2 (de) 1975-07-10
GB1028465A (en) 1966-05-04

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Legal Events

Date Code Title Description
C2 Grant after previous publication (2nd publication)