FR2309729B1 - - Google Patents

Info

Publication number
FR2309729B1
FR2309729B1 FR7611709A FR7611709A FR2309729B1 FR 2309729 B1 FR2309729 B1 FR 2309729B1 FR 7611709 A FR7611709 A FR 7611709A FR 7611709 A FR7611709 A FR 7611709A FR 2309729 B1 FR2309729 B1 FR 2309729B1
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
FR7611709A
Other languages
French (fr)
Other versions
FR2309729A1 (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 Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2309729A1 publication Critical patent/FR2309729A1/fr
Application granted granted Critical
Publication of FR2309729B1 publication Critical patent/FR2309729B1/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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gasket Seals (AREA)
  • Connection Of Plates (AREA)
FR7611709A 1975-05-02 1976-04-21 Anneau collecteur de refrigerant pour propulseur-fusee Granted FR2309729A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19752519538 DE2519538C2 (de) 1975-05-02 1975-05-02 Verbindung zwischen dem Kühlmittel-Zulaufring und der Brennkammer-oder Schubdüsenwand eines Raketentriebwerks

Publications (2)

Publication Number Publication Date
FR2309729A1 FR2309729A1 (fr) 1976-11-26
FR2309729B1 true FR2309729B1 (enExample) 1980-04-18

Family

ID=5945560

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7611709A Granted FR2309729A1 (fr) 1975-05-02 1976-04-21 Anneau collecteur de refrigerant pour propulseur-fusee

Country Status (3)

Country Link
JP (1) JPS51133613A (enExample)
DE (1) DE2519538C2 (enExample)
FR (1) FR2309729A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10237381B4 (de) * 2002-08-12 2005-06-23 Eads Space Transportation Gmbh Brennkammerstruktur und Verfahren zu deren Herstellung
RU2465483C1 (ru) * 2011-03-31 2012-10-27 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") Способ изготовления сопла камеры сгорания жидкостного ракетного двигателя (жрд)
RU2519003C1 (ru) * 2013-04-09 2014-06-10 Открытое акционерное общество "Конструкторское бюро химавтоматики" Способ изготовления сопла камеры сгорания жидкостного ракетного двигателя
CN107940157B (zh) * 2017-11-20 2020-07-24 西安航天动力研究所 一种再生冷却燃气导管及其加工方法
CN108979900A (zh) * 2018-08-29 2018-12-11 北京航天动力研究所 一种液体火箭发动机推力室身部的集液环
CN118188222B (zh) * 2024-04-25 2024-10-11 陕西天回航天技术有限公司 双夹层再生冷却与液膜冷却的复合方法、系统及发动机推力室

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE562285A (enExample) * 1956-11-09
FR1232288A (fr) * 1957-06-21 1960-10-06 Bristol Siddeley Engines Ltd Perfectionnements aux chambres de combustion
US3001726A (en) * 1959-06-23 1961-09-26 United Aircraft Corp Manifold attachment
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
DE1751180A1 (de) * 1968-04-18 1971-04-29 Messerschmitt Boelkow Blohm Ausbildung und Anordnung eines Zulaufringes oder Ablaufsammelringes fuer Schubduesen oder Brennkammern von Raketentriebwerken,insbesondere Fluessigkeitsraketentriebwerken
DE6901525U (de) * 1969-01-16 1970-07-09 Messerschmitt Boelkow Blohm Vorrichtung zur verbindung des kuehlmitteleinlaufringes mit der wand einer raketenbrennkammer oder schubduese
DE1941296B2 (de) * 1969-08-14 1971-09-30 Messerschmitt Bolkow Blohm GmbH, 8000 München Durch ein fluessiges medium regenerativ gekuehlte brenn kammer mit schubduese
DE2356572C3 (de) * 1973-11-13 1979-03-29 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Flüssigkeitsgekühlte Raketenbrennkammer mit Schubdüse

Also Published As

Publication number Publication date
FR2309729A1 (fr) 1976-11-26
JPS51133613A (en) 1976-11-19
DE2519538C2 (de) 1982-12-30
DE2519538A1 (de) 1976-11-18

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Legal Events

Date Code Title Description
ST Notification of lapse