DE69624841D1 - Schubdüse eines raketentriebwerks - Google Patents

Schubdüse eines raketentriebwerks

Info

Publication number
DE69624841D1
DE69624841D1 DE69624841T DE69624841T DE69624841D1 DE 69624841 D1 DE69624841 D1 DE 69624841D1 DE 69624841 T DE69624841 T DE 69624841T DE 69624841 T DE69624841 T DE 69624841T DE 69624841 D1 DE69624841 D1 DE 69624841D1
Authority
DE
Germany
Prior art keywords
rocket engine
throttle nozzle
throttle
nozzle
rocket
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
DE69624841T
Other languages
English (en)
Other versions
DE69624841T2 (de
Inventor
Jan Haeggander
Lars-Olof Pekkari
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
Publication of DE69624841D1 publication Critical patent/DE69624841D1/de
Application granted granted Critical
Publication of DE69624841T2 publication Critical patent/DE69624841T2/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)
  • Testing Of Engines (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE69624841T 1996-02-12 1996-02-12 Schubdüse eines raketentriebwerks Expired - Lifetime DE69624841T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SE1996/000176 WO1997029277A1 (en) 1996-02-12 1996-02-12 Rocket engine nozzle

Publications (2)

Publication Number Publication Date
DE69624841D1 true DE69624841D1 (de) 2002-12-19
DE69624841T2 DE69624841T2 (de) 2003-09-04

Family

ID=20401062

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69624841T Expired - Lifetime DE69624841T2 (de) 1996-02-12 1996-02-12 Schubdüse eines raketentriebwerks

Country Status (5)

Country Link
US (1) US6176077B1 (de)
EP (1) EP0880645B1 (de)
JP (1) JP3875723B2 (de)
DE (1) DE69624841T2 (de)
WO (1) WO1997029277A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
UA46175C2 (uk) 1998-12-04 2002-05-15 Вольво Аеро Корпорейшн Профіль сопла ракетного двигуна, що уможливлює керування відривом потоку та забезпечує зменшення бічного навантаження
SE516049C2 (sv) * 2000-03-17 2001-11-12 Volvo Aero Corp Anordning för styrning av flödesseparationslinjen hos raketmunstycken
US6716077B1 (en) * 2000-05-17 2004-04-06 Micron Technology, Inc. Method of forming flow-fill structures
DE10123731C2 (de) 2001-05-15 2003-08-21 Astrium Gmbh Verfahren zur Verlängerung einer Düse und verlängerbare Düse für Raketentriebwerke
US6883220B2 (en) 2002-07-17 2005-04-26 The Boeing Company Method for forming a tube-walled article
JP2011069346A (ja) * 2009-09-25 2011-04-07 Kenji Ikeda ロケットロータリーハイブリットエンジン
CN110977618B (zh) * 2019-12-02 2021-01-12 西安航天发动机有限公司 钛合金喷管内壁划区域采集母线数据的方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1372515A (fr) * 1963-07-12 1964-09-18 Sud Aviation Perfectionnements apportés aux tuyères pour avions à réaction
US3292865A (en) * 1963-10-17 1966-12-20 Gen Motors Corp Thrust vector control with clustered nozzles
US4707899A (en) 1985-08-21 1987-11-24 Morton Thiokol, Inc. Method of making rocket motor extendible nozzle exit cone
US5343698A (en) 1993-04-28 1994-09-06 United Technologies Corporation Hexagonal cluster nozzle for a rocket engine

Also Published As

Publication number Publication date
JP2000504804A (ja) 2000-04-18
DE69624841T2 (de) 2003-09-04
US6176077B1 (en) 2001-01-23
EP0880645A1 (de) 1998-12-02
EP0880645B1 (de) 2002-11-13
JP3875723B2 (ja) 2007-01-31
WO1997029277A1 (en) 1997-08-14

Similar Documents

Publication Publication Date Title
DE69722877D1 (de) Aerodynamisches Einspritzsystem zur Einspritzung eines Brennstoff-Luft-Gemisches
FR2745355B1 (fr) Tuyau distributeur de carburant
NO307102B1 (no) Innsproeytningsventilarrangement for en forbrennintgotor
DE69409152D1 (de) Schubdüse eines Raketentriebwerkes
DE69625081D1 (de) Ausfahrbare raketentriebwerkdüse
DE69509821D1 (de) Ankeranordnung eines Kraftstoffeinspritzventils
ATA157695A (de) Viertakt-brennkraftmaschine
IT1294249B1 (it) Valvola di iniezione per motori a combustione
DE69624841D1 (de) Schubdüse eines raketentriebwerks
DE69425532D1 (de) Einlassvorrichtung einer Dieselkraftmaschine
ATE236344T1 (de) Rotierende brennkraftmaschine
FR2722540B1 (fr) Buse d'injection de carburant
DE69709806T2 (de) Brennkammer einer Dieselbrennkraftmaschine
DE69702840T2 (de) Vergaser brennstoffdüse
DE69418139D1 (de) Luftunterstütztes Einstrahlkraftstoffeinspritzventil
DE69814523D1 (de) Kraftstoffeinspritzanlage eines Dieselmotors
KR950019423U (ko) 디이젤 엔진의 분사노즐
KR970041545U (ko) 연료 분사 노즐
KR970041551U (ko) 엔진의 직접분사식 노즐
KR950033809U (ko) 석유연소기의 기화기 연료분사노즐
KR970055180U (ko) 연료 분사노즐의 구조
GB2301630B (en) Internal combustion turbine engine
KR970043865U (ko) 연소기기의 기화기 노즐
KR950014633U (ko) 간접분사방식 내연기관용 분사노즐
KR950019424U (ko) 디이젤 엔진의 연료 분사노즐

Legal Events

Date Code Title Description
8364 No opposition during term of opposition