FR2408037B1 - - Google Patents

Info

Publication number
FR2408037B1
FR2408037B1 FR7733442A FR7733442A FR2408037B1 FR 2408037 B1 FR2408037 B1 FR 2408037B1 FR 7733442 A FR7733442 A FR 7733442A FR 7733442 A FR7733442 A FR 7733442A FR 2408037 B1 FR2408037 B1 FR 2408037B1
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.)
Expired
Application number
FR7733442A
Other versions
FR2408037A1 (fr
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7733442A priority Critical patent/FR2408037A1/fr
Priority to IT29247/78A priority patent/IT1099864B/it
Priority to GB7842942A priority patent/GB2007773B/en
Priority to DE2848114A priority patent/DE2848114C3/de
Publication of FR2408037A1 publication Critical patent/FR2408037A1/fr
Application granted granted Critical
Publication of FR2408037B1 publication Critical patent/FR2408037B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
  • Toys (AREA)
  • General Induction Heating (AREA)
  • Woven Fabrics (AREA)
FR7733442A 1977-11-07 1977-11-07 Tuyere chaude Granted FR2408037A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7733442A FR2408037A1 (fr) 1977-11-07 1977-11-07 Tuyere chaude
IT29247/78A IT1099864B (it) 1977-11-07 1978-10-30 Ugello caldo
GB7842942A GB2007773B (en) 1977-11-07 1978-11-02 Nozzle for propulsion units
DE2848114A DE2848114C3 (de) 1977-11-07 1978-11-06 Heißdüse für Raketentriebwerke

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7733442A FR2408037A1 (fr) 1977-11-07 1977-11-07 Tuyere chaude

Publications (2)

Publication Number Publication Date
FR2408037A1 FR2408037A1 (fr) 1979-06-01
FR2408037B1 true FR2408037B1 (fr) 1981-11-27

Family

ID=9197340

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7733442A Granted FR2408037A1 (fr) 1977-11-07 1977-11-07 Tuyere chaude

Country Status (4)

Country Link
DE (1) DE2848114C3 (fr)
FR (1) FR2408037A1 (fr)
GB (1) GB2007773B (fr)
IT (1) IT1099864B (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2450356A1 (fr) * 1979-02-27 1980-09-26 Aerospatiale Agencement de pilotage d'un propulseur d'engin a propergol solide
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
US4967599A (en) * 1980-05-19 1990-11-06 Societe Europeenne De Propulsion Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor
FR2516609A1 (fr) * 1981-11-19 1983-05-20 Snecma Dispositif de fixation de deux pieces de revolution en materiaux ayant des coefficients de dilatation differents
RU2529749C1 (ru) * 2013-07-17 2014-09-27 Открытое акционерное общество Научно-производственное объединение "Искра" Установка для определения окислительной стойкости углерод-углеродного композиционного материала
RU2632393C1 (ru) * 2016-07-04 2017-10-04 Акционерное общество Центральный научно-исследовательский институт специального машиностроения Подвесной шарнир поворотного сопла из композиционных материалов и способ его изготовления

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3140584A (en) * 1959-05-07 1964-07-14 Thiokol Chemical Corp Steering device for rocket-powered vehicles
DE1203646B (de) * 1962-12-21 1965-10-21 Studebaker Corp Geschichtete, faserverstaerkte Kunststoffwandung fuer Flugkoerper, Raketenantriebe u. dgl.
FR1554059A (fr) * 1968-01-17 1969-01-17
US3826708A (en) * 1970-05-18 1974-07-30 Mc Donnell Douglas Corp Rocket nozzle liner construction
GB1334592A (en) * 1971-01-21 1973-10-24 Imp Metal Ind Kynoch Ltd Flexible duct assemblies
DE2350103A1 (de) * 1973-10-05 1975-04-10 Bayern Chemie Gmbh Flugchemie Schwenkduese an einem gasleitrohr eines raketentriebwerks

Also Published As

Publication number Publication date
GB2007773A (en) 1979-05-23
FR2408037A1 (fr) 1979-06-01
DE2848114C3 (de) 1981-07-09
DE2848114A1 (de) 1979-05-17
IT1099864B (it) 1985-09-28
IT7829247A0 (it) 1978-10-30
DE2848114B2 (de) 1980-10-16
GB2007773B (en) 1982-04-21

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Legal Events

Date Code Title Description
ST Notification of lapse