FR2622931B1 - Mecanisme d'actionnement de tuyere de poussee prolongeable de moteur-fusee - Google Patents

Mecanisme d'actionnement de tuyere de poussee prolongeable de moteur-fusee

Info

Publication number
FR2622931B1
FR2622931B1 FR8814655A FR8814655A FR2622931B1 FR 2622931 B1 FR2622931 B1 FR 2622931B1 FR 8814655 A FR8814655 A FR 8814655A FR 8814655 A FR8814655 A FR 8814655A FR 2622931 B1 FR2622931 B1 FR 2622931B1
Authority
FR
France
Prior art keywords
operation mechanism
rocket nozzle
nozzle operation
extendable
motor 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
FR8814655A
Other languages
English (en)
Other versions
FR2622931A1 (fr
Inventor
Werner Malburg
Erich Kirner
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 FR2622931A1 publication Critical patent/FR2622931A1/fr
Application granted granted Critical
Publication of FR2622931B1 publication Critical patent/FR2622931B1/fr
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)
FR8814655A 1987-11-10 1988-11-09 Mecanisme d'actionnement de tuyere de poussee prolongeable de moteur-fusee Expired - Lifetime FR2622931B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3738108 1987-11-10

Publications (2)

Publication Number Publication Date
FR2622931A1 FR2622931A1 (fr) 1989-05-12
FR2622931B1 true FR2622931B1 (fr) 1991-01-11

Family

ID=6340169

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8814655A Expired - Lifetime FR2622931B1 (fr) 1987-11-10 1988-11-09 Mecanisme d'actionnement de tuyere de poussee prolongeable de moteur-fusee

Country Status (1)

Country Link
FR (1) FR2622931B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2677080B1 (fr) * 1991-05-30 1995-01-06 Europ Propulsion Mecanisme autoverrouillable et reversible de deploiement de divergent de tuyere de moteur-fusee.
FR2743110B1 (fr) * 1995-12-28 1998-03-27 Europ Propulsion Divergent deployable de 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
FR2944063B1 (fr) 2009-04-02 2014-04-25 Snecma Divergent deployable de propulseur
FR2989354B1 (fr) * 2012-04-13 2014-05-23 Snecma Etage de lanceur comprenant une structure de support temporaire de troncons de tuyere, permettant l'acces au corps du moteur

Also Published As

Publication number Publication date
FR2622931A1 (fr) 1989-05-12

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Legal Events

Date Code Title Description
ST Notification of lapse