GB1345257A - Jet propulsopm imots - Google Patents

Jet propulsopm imots

Info

Publication number
GB1345257A
GB1345257A GB2490971*A GB2490971A GB1345257A GB 1345257 A GB1345257 A GB 1345257A GB 2490971 A GB2490971 A GB 2490971A GB 1345257 A GB1345257 A GB 1345257A
Authority
GB
United Kingdom
Prior art keywords
nozzle
apertures
thrust
propulsopm
imots
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
GB2490971*A
Other languages
English (en)
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 GB1345257A publication Critical patent/GB1345257A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket 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)
  • Nozzles (AREA)
  • Jet Pumps And Other Pumps (AREA)
GB2490971*A 1970-05-08 1971-04-19 Jet propulsopm imots Expired GB1345257A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB1345257A true GB1345257A (en) 1974-01-30

Family

ID=5770583

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2490971*A Expired GB1345257A (en) 1970-05-08 1971-04-19 Jet propulsopm imots

Country Status (4)

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

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2949522C2 (de) * 1979-12-08 1982-01-28 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Gekühlte Schubdüse für ein Raketentriebwerk
FR2618488B1 (fr) * 1987-07-20 1989-12-15 Europ Propulsion Divergent a rupture de galbe pour tuyere de moteur-fusee
US5619851A (en) * 1989-02-08 1997-04-15 United Technologies Corporation Rocket nozzle for a rocket engine
US5683033A (en) * 1989-02-08 1997-11-04 United Technologies Corporation Rocket nozzle for a rocket engine
DE3905748A1 (de) * 1989-02-24 1993-06-03 Dornier Gmbh Scheinziel
WO2000032920A1 (en) * 1998-11-27 2000-06-08 Volvo Aero Corporation Nozzle structure for rocket nozzles having cooled nozzle wall
SE516049C2 (sv) * 2000-03-17 2001-11-12 Volvo Aero Corp Anordning för styrning av flödesseparationslinjen hos raketmunstycken
SE516046C2 (sv) 2000-03-17 2001-11-12 Volvo Aero Corp Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp
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

Also Published As

Publication number Publication date
FR2088412A7 (enExample) 1972-01-07
FR2088412B3 (enExample) 1973-12-28
DE2022517A1 (de) 1971-11-25
US3712546A (en) 1973-01-23

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees