FR2199578A1 - - Google Patents

Info

Publication number
FR2199578A1
FR2199578A1 FR7327420A FR7327420A FR2199578A1 FR 2199578 A1 FR2199578 A1 FR 2199578A1 FR 7327420 A FR7327420 A FR 7327420A FR 7327420 A FR7327420 A FR 7327420A FR 2199578 A1 FR2199578 A1 FR 2199578A1
Authority
FR
France
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.)
Granted
Application number
FR7327420A
Other languages
French (fr)
Other versions
FR2199578B1 (enExample
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.)
Aerojet Rocketdyne Inc
Original Assignee
Aerojet General Corp
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 Aerojet General Corp filed Critical Aerojet General Corp
Publication of FR2199578A1 publication Critical patent/FR2199578A1/fr
Application granted granted Critical
Publication of FR2199578B1 publication Critical patent/FR2199578B1/fr
Expired 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
FR7327420A 1972-07-26 1973-07-26 Expired FR2199578B1 (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US275379A US3860134A (en) 1972-07-26 1972-07-26 Flexible nozzle for a thrust vector control system

Publications (2)

Publication Number Publication Date
FR2199578A1 true FR2199578A1 (enExample) 1974-04-12
FR2199578B1 FR2199578B1 (enExample) 1976-04-30

Family

ID=23052043

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7327420A Expired FR2199578B1 (enExample) 1972-07-26 1973-07-26

Country Status (6)

Country Link
US (1) US3860134A (enExample)
JP (1) JPS4985798A (enExample)
CA (1) CA982194A (enExample)
DE (1) DE2337193A1 (enExample)
FR (1) FR2199578B1 (enExample)
IT (1) IT989951B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5399309A (en) * 1985-12-11 1995-03-21 Thiokol Corporation Tape wrapped, fabric reinforced, flex bearing
US5786285A (en) * 1996-05-14 1998-07-28 United Technologies Corporation Elastomer coated layer for erosion and/or fire protection
FR2777322B1 (fr) * 1998-04-09 2000-07-07 Snecma Dispositif d'ancrage pour un organe d'activation de tuyere orientable
US6981365B1 (en) * 2001-12-28 2006-01-03 Sierra Engineering Incorporated Supersonic revolving nozzle
US20070295857A1 (en) * 2005-11-16 2007-12-27 Lloyd Peter G Emergency Device
US7966828B2 (en) * 2007-01-08 2011-06-28 United Technologies Corporation Variable area nozzle with woven sleeve extension
US8696033B2 (en) * 2011-07-15 2014-04-15 Aerojet Rocketdyne Of De, Inc. Scissor duct flex joint damper
RU2539236C1 (ru) * 2013-12-25 2015-01-20 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Корпус раструба поворотного сопла из композиционных материалов
US10072613B2 (en) 2015-02-23 2018-09-11 Orbital Atk, Inc. Methods of forming flexible structures for a rocket motor assembly, related flexible structures, and related assemblies including the flexible structures
US10815936B2 (en) 2016-11-09 2020-10-27 Northrop Grumman Innovation Systems, Inc. Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearings
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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1352892A (fr) * 1962-12-21 1964-02-21 Studebaker Corp éléments à parois stratifiées en contact avec une circulation de fluide animée d'une vitesse élevée
FR1414824A (fr) * 1964-07-24 1965-10-22 Snecma Dispositif de liaison déformable et son application aux fusées
US3270503A (en) * 1965-01-13 1966-09-06 Jr Andre J Meyer Ablation structures
US3573123A (en) * 1966-05-11 1971-03-30 United Aircraft Corp Composite high temperature resistant material and method of fabrication

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703109A (en) * 1951-08-25 1955-03-01 Gen Dynamics Corp Duct construction
US3249306A (en) * 1962-09-14 1966-05-03 Aerojet General Co Automatically adjustable rocket nozzle
US3482783A (en) * 1966-08-12 1969-12-09 Goodyear Aerospace Corp Expandable nozzle
US3534908A (en) * 1967-11-02 1970-10-20 North American Rockwell Variable geometry nozzle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1352892A (fr) * 1962-12-21 1964-02-21 Studebaker Corp éléments à parois stratifiées en contact avec une circulation de fluide animée d'une vitesse élevée
FR1414824A (fr) * 1964-07-24 1965-10-22 Snecma Dispositif de liaison déformable et son application aux fusées
US3270503A (en) * 1965-01-13 1966-09-06 Jr Andre J Meyer Ablation structures
US3573123A (en) * 1966-05-11 1971-03-30 United Aircraft Corp Composite high temperature resistant material and method of fabrication

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
EP0029773A1 (fr) * 1979-11-23 1981-06-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Tuyère orientable pour propulseur à réaction
US4363445A (en) * 1979-11-23 1982-12-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Thrust-vectoring nozzle for jet propulsion system

Also Published As

Publication number Publication date
FR2199578B1 (enExample) 1976-04-30
IT989951B (it) 1975-06-10
JPS4985798A (enExample) 1974-08-16
CA982194A (en) 1976-01-20
DE2337193A1 (de) 1974-02-07
US3860134A (en) 1975-01-14

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Legal Events

Date Code Title Description
ST Notification of lapse