FR1322872A - Method and device for deflecting the jet of a rocket - Google Patents

Method and device for deflecting the jet of a rocket

Info

Publication number
FR1322872A
FR1322872A FR887391A FR887391A FR1322872A FR 1322872 A FR1322872 A FR 1322872A FR 887391 A FR887391 A FR 887391A FR 887391 A FR887391 A FR 887391A FR 1322872 A FR1322872 A FR 1322872A
Authority
FR
France
Prior art keywords
rocket
deflecting
jet
Prior art date
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.)
Expired
Application number
FR887391A
Other languages
French (fr)
Inventor
Henri Bertin Et Cyrille F Jean
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.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie SA
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 Bertin et Cie SA filed Critical Bertin et Cie SA
Priority to FR887391A priority Critical patent/FR1322872A/en
Priority to US255938A priority patent/US3233833A/en
Priority to DE1963S0083648 priority patent/DE1240747C2/en
Priority to GB519163A priority patent/GB1028465A/en
Application granted granted Critical
Publication of FR1322872A publication Critical patent/FR1322872A/en
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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
FR887391A 1962-02-08 1962-02-08 Method and device for deflecting the jet of a rocket Expired FR1322872A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR887391A FR1322872A (en) 1962-02-08 1962-02-08 Method and device for deflecting the jet of a rocket
US255938A US3233833A (en) 1962-02-08 1963-02-04 Method and device for deflecting a rocket jet
DE1963S0083648 DE1240747C2 (en) 1962-02-08 1963-02-07 JET THROTTLE FOR HOT GASES WITH JET DEFLECTION DUE TO THE INTRODUCTION OF AN AUXILIARY FLUID
GB519163A GB1028465A (en) 1962-02-08 1963-02-08 Method of deflecting a hot gas jet passing through a nozzle for carrying out the method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR887391A FR1322872A (en) 1962-02-08 1962-02-08 Method and device for deflecting the jet of a rocket

Publications (1)

Publication Number Publication Date
FR1322872A true FR1322872A (en) 1963-04-05

Family

ID=8772250

Family Applications (1)

Application Number Title Priority Date Filing Date
FR887391A Expired FR1322872A (en) 1962-02-08 1962-02-08 Method and device for deflecting the jet of a rocket

Country Status (2)

Country Link
US (1) US3233833A (en)
FR (1) FR1322872A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1391927A (en) * 1964-01-29 1965-03-12 Monsieur Le Ministre Des Armee Combustion chamber with nozzle for liquid rocket engines
DE1475163A1 (en) * 1964-10-19 1969-01-23 Dynamit Nobel Ag Method and device for atomizing liquids, solutions, suspensions or solids in the form of dust, powder or the like.
US3353356A (en) * 1965-06-14 1967-11-21 Thiokol Chemical Corp Vector control system, which includes means for introducing an auxiliary exhaust stream into the primary stream of a rocket motor
US3465966A (en) * 1966-02-16 1969-09-09 Thiokol Chemical Corp Rocket control
US3491539A (en) * 1967-07-13 1970-01-27 Thiokol Chemical Corp Injector assembly for eliminating the smoke trail of a solid propellant rocket motor
US3481543A (en) * 1967-12-18 1969-12-02 Thiokol Chemical Corp Rocket thrust nozzle
GB1293232A (en) * 1969-07-28 1972-10-18 Aerospatiale Fluid discharge nozzles having means for deflecting the flow of fluid discharged
DE3009671A1 (en) * 1980-03-13 1981-09-24 Schottel-Werft Josef Becker Gmbh & Co Kg, 5401 Spay WATERJET DRIVE DEVICE FOR DRIVING WATER VEHICLES
US6568171B2 (en) * 2001-07-05 2003-05-27 Aerojet-General Corporation Rocket vehicle thrust augmentation within divergent section of nozzle
US7823376B2 (en) * 2005-09-13 2010-11-02 Aerojet-General Corporation Thrust augmentation in plug nozzles and expansion-deflection nozzles
US7775460B2 (en) * 2006-10-24 2010-08-17 United Technologies Corporation Combustion nozzle fluidic injection assembly
CN104712462B (en) * 2015-01-14 2016-06-08 北京理工大学 A kind of a secondary fluid jet thrust adjusting device of replaceable jet pipe

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2405785A (en) * 1944-03-14 1946-08-13 Daniel And Florence Guggenheim Combustion chamber
US2943821A (en) * 1950-12-30 1960-07-05 United Aircraft Corp Directional control means for a supersonic vehicle
US2952123A (en) * 1956-05-25 1960-09-13 Lockheed Aircraft Corp Directional controls for propulsive jets
FR1182810A (en) * 1957-09-16 1959-06-30 Snecma Improvements to adjustable section ejection nozzles
US3066485A (en) * 1957-12-11 1962-12-04 Bertin & Cie Steering device for rocket-propelled vehicles
US3091924A (en) * 1960-12-15 1963-06-04 United Aircraft Corp Gaseous nozzle boundary
US3092963A (en) * 1960-12-15 1963-06-11 United Aircraft Corp Vector control system

Also Published As

Publication number Publication date
US3233833A (en) 1966-02-08

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