FR2088412A7 - - Google Patents

Info

Publication number
FR2088412A7
FR2088412A7 FR7110803A FR7110803A FR2088412A7 FR 2088412 A7 FR2088412 A7 FR 2088412A7 FR 7110803 A FR7110803 A FR 7110803A FR 7110803 A FR7110803 A FR 7110803A FR 2088412 A7 FR2088412 A7 FR 2088412A7
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
FR7110803A
Other languages
French (fr)
Other versions
FR2088412B3 (OSRAM
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
Application granted granted Critical
Publication of FR2088412A7 publication Critical patent/FR2088412A7/fr
Publication of FR2088412B3 publication Critical patent/FR2088412B3/fr
Expired 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
    • F02K9/97—Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Processing Of Solid Wastes (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Nozzles (AREA)
FR7110803A 1970-05-08 1971-03-26 Expired FR2088412B3 (OSRAM)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702022517 DE2022517A1 (de) 1970-05-08 1970-05-08 Raketentriebwerksduese mit Grenzschichtabsaugung

Publications (2)

Publication Number Publication Date
FR2088412A7 true FR2088412A7 (OSRAM) 1972-01-07
FR2088412B3 FR2088412B3 (OSRAM) 1973-12-28

Family

ID=5770583

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7110803A Expired FR2088412B3 (OSRAM) 1970-05-08 1971-03-26

Country Status (4)

Country Link
US (1) US3712546A (OSRAM)
DE (1) DE2022517A1 (OSRAM)
FR (1) FR2088412B3 (OSRAM)
GB (1) GB1345257A (OSRAM)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2471486A1 (fr) * 1979-12-08 1981-06-19 Messerschmitt Boelkow Blohm Dispositif pour le refroidissement de la tuyere de poussee d'un propulseur-fusee
FR2618488A1 (fr) * 1987-07-20 1989-01-27 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
FR2687774A1 (fr) * 1989-02-24 1993-08-27 Dornier Gmbh Cible factice.

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5683033A (en) * 1989-02-08 1997-11-04 United Technologies Corporation Rocket nozzle for a rocket engine
US5619851A (en) * 1989-02-08 1997-04-15 United Technologies Corporation Rocket nozzle for a rocket engine
US6467253B1 (en) 1998-11-27 2002-10-22 Volvo Aero Corporation Nozzle structure for rocket nozzles having cooled nozzle wall
SE516046C2 (sv) * 2000-03-17 2001-11-12 Volvo Aero Corp Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp
SE516049C2 (sv) * 2000-03-17 2001-11-12 Volvo Aero Corp Anordning för styrning av flödesseparationslinjen hos raketmunstycken
GB2398046B (en) * 2003-01-15 2006-07-12 S & C Thermofluids Ltd The use of porous surfaces with coanda effect
RU2551244C2 (ru) * 2013-07-16 2015-05-20 Федеральное государственное бюджетное учреждение науки Институт теоретической и прикладной механики им. С.А. Христиановича Сибирского отделения Российской академии наук (ИТПМ СО РАН) Способ увеличения тяги сверхзвукового сопла ракетного двигателя
CN116696593A (zh) * 2023-06-25 2023-09-05 哈尔滨工程大学 一种用于可渗透喷管的轻质多孔介质夹层结构

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2481059A (en) * 1944-08-28 1949-09-06 Us Sec War Adjustable rocket nozzle
FR1273933A (fr) * 1960-09-06 1961-10-20 Terseram Soc Nouv Dispositif de sécurité pour tuyère de fusée
US3092963A (en) * 1960-12-15 1963-06-11 United Aircraft Corp Vector control system
US3134224A (en) * 1961-05-26 1964-05-26 United Aircraft Corp Gas bleed from rocket chamber
US3230705A (en) * 1962-07-11 1966-01-25 Trw Inc Chemically cooled rocket
US3224678A (en) * 1962-10-04 1965-12-21 Marquardt Corp Modular thrust chamber
US3297256A (en) * 1965-07-08 1967-01-10 Frederick R Hickerson Thrust controlled rocket motor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2471486A1 (fr) * 1979-12-08 1981-06-19 Messerschmitt Boelkow Blohm Dispositif pour le refroidissement de la tuyere de poussee d'un propulseur-fusee
FR2618488A1 (fr) * 1987-07-20 1989-01-27 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
US4947644A (en) * 1987-07-20 1990-08-14 Societe Europeenne De Propulsion Diverging portion of discontinuous curvature for a rocket engine nozzle
FR2687774A1 (fr) * 1989-02-24 1993-08-27 Dornier Gmbh Cible factice.

Also Published As

Publication number Publication date
GB1345257A (en) 1974-01-30
FR2088412B3 (OSRAM) 1973-12-28
US3712546A (en) 1973-01-23
DE2022517A1 (de) 1971-11-25

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Legal Events

Date Code Title Description
ST Notification of lapse