DE60108015D1 - Einrichtung zur beeinflussung der ablösungsgrenze bei raketendüsen - Google Patents

Einrichtung zur beeinflussung der ablösungsgrenze bei raketendüsen

Info

Publication number
DE60108015D1
DE60108015D1 DE60108015T DE60108015T DE60108015D1 DE 60108015 D1 DE60108015 D1 DE 60108015D1 DE 60108015 T DE60108015 T DE 60108015T DE 60108015 T DE60108015 T DE 60108015T DE 60108015 D1 DE60108015 D1 DE 60108015D1
Authority
DE
Germany
Prior art keywords
raket
needles
influencing
discharge limit
discharge
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 - Lifetime
Application number
DE60108015T
Other languages
English (en)
Other versions
DE60108015T2 (de
Inventor
Arne Boman
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.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero AB
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 Volvo Aero AB filed Critical Volvo Aero AB
Application granted granted Critical
Publication of DE60108015D1 publication Critical patent/DE60108015D1/de
Publication of DE60108015T2 publication Critical patent/DE60108015T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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)
  • Nozzles (AREA)
  • Testing Of Engines (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE60108015T 2000-03-17 2001-03-16 Einrichtung zur beeinflussung der ablösungsgrenze bei raketendüsen Expired - Lifetime DE60108015T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE0000896A SE516049C2 (sv) 2000-03-17 2000-03-17 Anordning för styrning av flödesseparationslinjen hos raketmunstycken
SE0000896 2000-03-17
PCT/SE2001/000554 WO2001069069A1 (en) 2000-03-17 2001-03-16 An apparatus for controlling the flow separation line of rocket nozzles

Publications (2)

Publication Number Publication Date
DE60108015D1 true DE60108015D1 (de) 2005-02-03
DE60108015T2 DE60108015T2 (de) 2005-12-08

Family

ID=20278855

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60108015T Expired - Lifetime DE60108015T2 (de) 2000-03-17 2001-03-16 Einrichtung zur beeinflussung der ablösungsgrenze bei raketendüsen

Country Status (11)

Country Link
US (1) US6574952B2 (de)
EP (1) EP1179131B1 (de)
JP (1) JP4570309B2 (de)
CN (1) CN1177999C (de)
AU (1) AU4294101A (de)
DE (1) DE60108015T2 (de)
ES (1) ES2233616T3 (de)
RU (1) RU2262613C2 (de)
SE (1) SE516049C2 (de)
UA (1) UA69452C2 (de)
WO (1) WO2001069069A1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080098741A1 (en) * 2006-10-25 2008-05-01 United Technologies Corporation Annular isolator dual mode scramjet engine
US20080264372A1 (en) * 2007-03-19 2008-10-30 Sisk David B Two-stage ignition system
CN103444556B (zh) * 2013-08-17 2014-10-15 东瑞食品集团有限公司 一种高床发酵型养猪系统

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2022517A1 (de) * 1970-05-08 1971-11-25 Messerschmitt Boelkow Blohm Raketentriebwerksduese mit Grenzschichtabsaugung
US3925982A (en) * 1973-09-11 1975-12-16 Martin Marietta Corp Fluid-dynamic shock ring for controlled flow separation in a rocket engine exhaust nozzle
US5619851A (en) * 1989-02-08 1997-04-15 United Technologies Corporation Rocket nozzle for a rocket engine
FR2691209B1 (fr) 1992-05-18 1995-09-01 Europ Propulsion Enceinte contenant des gaz chauds refroidie par transpiration, notamment chambre propulsive de moteur-fusee, et procede de fabrication.
FR2705737B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à divergent échancré.
JP3875723B2 (ja) * 1996-02-12 2007-01-31 ボルボ エアロ コーポレイション ロケットエンジンノズル

Also Published As

Publication number Publication date
JP4570309B2 (ja) 2010-10-27
US20020152752A1 (en) 2002-10-24
CN1364217A (zh) 2002-08-14
CN1177999C (zh) 2004-12-01
EP1179131A1 (de) 2002-02-13
ES2233616T3 (es) 2005-06-16
UA69452C2 (uk) 2004-09-15
SE0000896L (sv) 2001-09-18
SE516049C2 (sv) 2001-11-12
EP1179131B1 (de) 2004-12-29
DE60108015T2 (de) 2005-12-08
RU2262613C2 (ru) 2005-10-20
SE0000896D0 (sv) 2000-03-17
US6574952B2 (en) 2003-06-10
JP2003527528A (ja) 2003-09-16
WO2001069069A1 (en) 2001-09-20
AU4294101A (en) 2001-09-24

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition