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DE69414086D1 - Rakete - Google Patents

Rakete

Info

Publication number
DE69414086D1
DE69414086D1 DE69414086T DE69414086T DE69414086D1 DE 69414086 D1 DE69414086 D1 DE 69414086D1 DE 69414086 T DE69414086 T DE 69414086T DE 69414086 T DE69414086 T DE 69414086T DE 69414086 D1 DE69414086 D1 DE 69414086D1
Authority
DE
Germany
Prior art keywords
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
DE69414086T
Other languages
English (en)
Other versions
DE69414086T2 (de
Inventor
Kenji C O Nagoya Gui Kishimoto
Yojiro Kakuma
Masaaki Yasui
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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
Priority claimed from JP5327380A external-priority patent/JP3029960B2/ja
Priority claimed from JP10260094A external-priority patent/JP3637076B2/ja
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Application granted granted Critical
Publication of DE69414086D1 publication Critical patent/DE69414086D1/de
Publication of DE69414086T2 publication Critical patent/DE69414086T2/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
    • F02K9/976—Deployable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
DE69414086T 1993-12-24 1994-12-13 Rakete Expired - Lifetime DE69414086T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP5327380A JP3029960B2 (ja) 1993-12-24 1993-12-24 ロケットエンジンの伸展ノズル機構
JP10260094A JP3637076B2 (ja) 1994-05-17 1994-05-17 伸展型の高膨張ノズルを備えたロケットエンジン

Publications (2)

Publication Number Publication Date
DE69414086D1 true DE69414086D1 (de) 1998-11-26
DE69414086T2 DE69414086T2 (de) 1999-05-12

Family

ID=26443286

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69414086T Expired - Lifetime DE69414086T2 (de) 1993-12-24 1994-12-13 Rakete

Country Status (3)

Country Link
US (1) US5641123A (de)
EP (1) EP0661436B1 (de)
DE (1) DE69414086T2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2757571B1 (fr) * 1996-12-24 2003-03-28 Europ Propulsion Divergent deployable pour propulseur
DE10123731C2 (de) * 2001-05-15 2003-08-21 Astrium Gmbh Verfahren zur Verlängerung einer Düse und verlängerbare Düse für Raketentriebwerke
DE10312776B4 (de) * 2003-03-21 2008-10-02 Eads Space Transportation Gmbh Ausfahrbare Schubdüsenglocke für ein Raketentriebwerk
DE102005039742B4 (de) * 2005-08-23 2008-10-02 Technische Universität Dresden Schubdüse für Raketen mit ausfahrbarer Düsenverlängerung
KR100998539B1 (ko) * 2008-08-29 2010-12-07 국방과학연구소 미사일의 구속해제장치
FR2944063B1 (fr) * 2009-04-02 2014-04-25 Snecma Divergent deployable de propulseur
FR2946095B1 (fr) 2009-05-27 2011-07-08 Snecma Piece de fixation entre la partie mobile d'un divergent deployable de propulseur et un mecanisme de deploiement de cette partie mobile
FR2975730B1 (fr) * 2011-05-23 2013-06-21 Snecma Systeme de reduction de la dynamique du segment mobile d'une tuyere deployable pour moteur de fusee
FR2998022B1 (fr) 2012-11-15 2015-01-16 Snecma Tige filetee d'un systeme de deploiement d'un divergent deployable de propulseur
CN113153581B (zh) * 2021-04-28 2022-11-15 哈尔滨工程大学 一种使用可延展材料包覆充流管道结构的柔性双钟型喷管

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049832A (en) * 1958-04-22 1962-08-21 Park Plastics Co Inc Two-stage rocket
US3218974A (en) * 1964-03-24 1965-11-23 Samms Adolphus Air breathing booster
US3561679A (en) * 1968-06-25 1971-02-09 Sam E Lager Collapsible nozzle for aircraft rocket motors
US3565208A (en) * 1970-02-02 1971-02-23 Rohr Corp Retractable silencing shield for jet engine nozzle
US4162040A (en) * 1975-12-03 1979-07-24 Textron Inc. Extendible/expandable nozzle for rocket engines and the like and method of making same
US4213566A (en) * 1978-08-25 1980-07-22 Hercules Incorporated Nested cone extendible nozzle system for a rocket motor
US4383407A (en) * 1981-02-02 1983-05-17 Thiokol Corporation Extendible thrust nozzle for rockets
JPS6050259A (ja) * 1983-08-29 1985-03-19 Nissan Motor Co Ltd ロケットモ−タのノズル構造
US4706886A (en) * 1984-08-27 1987-11-17 Rockwell International Corporation Extendible rocket-engine nozzle

Also Published As

Publication number Publication date
EP0661436B1 (de) 1998-10-21
US5641123A (en) 1997-06-24
DE69414086T2 (de) 1999-05-12
EP0661436A1 (de) 1995-07-05

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition