DE69202723T2 - Schockdämpfer für ein Strahlantriebssystem. - Google Patents

Schockdämpfer für ein Strahlantriebssystem.

Info

Publication number
DE69202723T2
DE69202723T2 DE1992602723 DE69202723T DE69202723T2 DE 69202723 T2 DE69202723 T2 DE 69202723T2 DE 1992602723 DE1992602723 DE 1992602723 DE 69202723 T DE69202723 T DE 69202723T DE 69202723 T2 DE69202723 T2 DE 69202723T2
Authority
DE
Germany
Prior art keywords
shock absorber
propulsion system
jet propulsion
jet
absorber
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 - Fee Related
Application number
DE1992602723
Other languages
English (en)
Other versions
DE69202723D1 (de
Inventor
Pascal Garnero
Roland Siegwald
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69202723D1 publication Critical patent/DE69202723D1/de
Application granted granted Critical
Publication of DE69202723T2 publication Critical patent/DE69202723T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/38—Safety devices, e.g. to prevent accidental ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Dampers (AREA)
  • Testing Of Engines (AREA)
  • Fluid-Damping Devices (AREA)
DE1992602723 1991-04-10 1992-03-25 Schockdämpfer für ein Strahlantriebssystem. Expired - Fee Related DE69202723T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9104365A FR2675207B1 (fr) 1991-04-10 1991-04-10 Systeme a debit de fluide a mise en pression brutale, notamment systeme de propulsion, muni d'un amortisseur d'onde de choc instationnaire.

Publications (2)

Publication Number Publication Date
DE69202723D1 DE69202723D1 (de) 1995-07-06
DE69202723T2 true DE69202723T2 (de) 1995-10-19

Family

ID=9411676

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1992602723 Expired - Fee Related DE69202723T2 (de) 1991-04-10 1992-03-25 Schockdämpfer für ein Strahlantriebssystem.

Country Status (6)

Country Link
EP (1) EP0508851B1 (de)
BR (1) BR9201282A (de)
DE (1) DE69202723T2 (de)
DK (1) DK0508851T3 (de)
ES (1) ES2072723T3 (de)
FR (1) FR2675207B1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2882401B1 (fr) * 2005-02-22 2007-05-11 Agence Spatiale Europeenne Dispositif et procede pour reduire les forces laterales non stationnaires agissant sur une tuyere d'un moteur de fusee
FR2882402B1 (fr) * 2005-02-22 2011-08-19 Agence Spatiale Europeenne Dispositif et procede pour reduire les forces laterales non stationnaires agissant sur une tuyere d'un moteur de fusee

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3115010A (en) * 1960-12-12 1963-12-24 Thiokol Chemical Corp Closure for container
US4033121A (en) * 1974-06-28 1977-07-05 The United States Of America As Represented By The Secretary Of The Army Noise controllable nozzle closure
GB1468814A (en) * 1974-12-03 1977-03-30 Secr Defence Rocket propulsion motors
GB2014664B (en) * 1978-02-15 1982-07-14 Secr Defence Shock wave attenuators

Also Published As

Publication number Publication date
DE69202723D1 (de) 1995-07-06
EP0508851A1 (de) 1992-10-14
BR9201282A (pt) 1992-12-01
EP0508851B1 (de) 1995-05-31
DK0508851T3 (da) 1995-07-31
FR2675207A1 (fr) 1992-10-16
FR2675207B1 (fr) 1995-03-03
ES2072723T3 (es) 1995-07-16

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DE69202723D1 (de) Schockdämpfer für ein Strahlantriebssystem.

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee