FR2863665B1 - Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur - Google Patents

Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur

Info

Publication number
FR2863665B1
FR2863665B1 FR8813413A FR8813413A FR2863665B1 FR 2863665 B1 FR2863665 B1 FR 2863665B1 FR 8813413 A FR8813413 A FR 8813413A FR 8813413 A FR8813413 A FR 8813413A FR 2863665 B1 FR2863665 B1 FR 2863665B1
Authority
FR
France
Prior art keywords
statoreactor
propulated
tubular
missile structure
missile
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
FR8813413A
Other languages
English (en)
Other versions
FR2863665A1 (fr
Inventor
Alain Chevalier
Thierry Hachin
Jacques Raynaud
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
Priority to FR8813413A priority Critical patent/FR2863665B1/fr
Priority to CA000611851A priority patent/CA1341492C/fr
Priority to SE8903302A priority patent/SE8903302D0/xx
Priority to DE3934071A priority patent/DE3934071B3/de
Priority to GB8922949A priority patent/GB2411438B/en
Priority to US07/421,633 priority patent/US8079308B1/en
Publication of FR2863665A1 publication Critical patent/FR2863665A1/fr
Application granted granted Critical
Publication of FR2863665B1 publication Critical patent/FR2863665B1/fr
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
    • F02K9/08—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
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02K9/24—Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/10—Application in ram-jet engines or ram-jet driven vehicles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)
  • Tents Or Canopies (AREA)
  • Laminated Bodies (AREA)
FR8813413A 1988-10-12 1988-10-12 Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur Expired - Fee Related FR2863665B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR8813413A FR2863665B1 (fr) 1988-10-12 1988-10-12 Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur
CA000611851A CA1341492C (fr) 1988-10-12 1989-09-19 Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur
SE8903302A SE8903302D0 (sv) 1988-10-12 1989-10-09 Drivanordning
DE3934071A DE3934071B3 (de) 1988-10-12 1989-10-12 Staustrahltriebwerk mit Rohrstruktur und durch ein solches Staustrahltriebwerk antreibbare Flugkörper
GB8922949A GB2411438B (en) 1988-10-12 1989-10-12 Improvements in or relating to ramjets
US07/421,633 US8079308B1 (en) 1988-10-12 1989-10-12 Ramjet engine incorporating a tubular structure and a missile propelled by a ramjet engines of this type

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8813413A FR2863665B1 (fr) 1988-10-12 1988-10-12 Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur

Publications (2)

Publication Number Publication Date
FR2863665A1 FR2863665A1 (fr) 2005-06-17
FR2863665B1 true FR2863665B1 (fr) 2007-03-30

Family

ID=9370945

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8813413A Expired - Fee Related FR2863665B1 (fr) 1988-10-12 1988-10-12 Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur

Country Status (6)

Country Link
US (1) US8079308B1 (fr)
CA (1) CA1341492C (fr)
DE (1) DE3934071B3 (fr)
FR (1) FR2863665B1 (fr)
GB (1) GB2411438B (fr)
SE (1) SE8903302D0 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8056319B2 (en) * 2006-11-10 2011-11-15 Aerojet—General Corporation Combined cycle missile engine system
JP6183836B2 (ja) * 2013-08-12 2017-08-23 株式会社Ｉｈｉエアロスペース ポートカバー開口装置
CN110195665B (zh) * 2019-06-21 2020-06-05 北京理工大学 一种再装填的储气式固体推进剂动力装置
US11796291B2 (en) * 2022-01-11 2023-10-24 Raytheon Company Effector having morphing airframe and method

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB590177A (en) * 1944-07-17 1947-07-10 Hydran Products Ltd Improvements in or relating to projectiles of the rocket type
US2835107A (en) * 1956-12-21 1958-05-20 Haveg Industries Inc Resins and use thereof
US2935946A (en) * 1957-07-19 1960-05-10 Elia A Gallo Telescoping ram jet construction
US3173249A (en) * 1959-08-10 1965-03-16 Thiokol Chemical Corp Air-breathing solid propellant ducted rocket
GB953260A (en) * 1961-01-04 1964-03-25 Thiokol Chemical Corp Air-breathing solid propellant ducted rocket
US3267662A (en) * 1962-11-20 1966-08-23 Atlantic Res Corp Fluid venting device
US3768255A (en) * 1967-03-06 1973-10-30 Texaco Inc Inlet port covers for reaction vehicle
SE340417B (fr) * 1969-06-06 1971-11-15 Bofors Ab
FR2230490A1 (en) * 1973-05-25 1974-12-20 Hercules Inc Filament wound vessel - having inner and outer loosely fitting shells
GB1417350A (en) * 1973-05-31 1975-12-10 Hercules Inc Filament wound vessel and method of manufacture
US3844118A (en) * 1973-08-28 1974-10-29 Us Air Force Aft inlet ramjet powered missile
JPS5844518B2 (ja) * 1976-09-03 1983-10-04 ダイセル化学工業株式会社 ロケツトの外殻体
FR2402773A1 (fr) * 1977-09-07 1979-04-06 Europ Propulsion Chambre de combustion de stato-fusee a booster integre
US4417441A (en) * 1979-03-29 1983-11-29 Messerschmitt-Bokow-Blohm Gesellschaft mit beschrankter Haftung Ram jet engine
US4441312A (en) * 1979-06-22 1984-04-10 The United States Of America As Represented By The Secretary Of The Air Force Combined cycle ramjet engine
DE2948197C2 (de) * 1979-11-30 1981-12-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Startschubdüse für Rückstoßtriebwerke, insbesondere Raketen-Staustrahltriebwerke
DE3002977C2 (de) * 1980-01-29 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Deckel aus leicht zerstörbarem Material zum Verschließen der in die Brennkammer von Staustrahl-Raketentriebwerken einmündenden Lufteinlauföffnungen, mit pyrotechnisch funktionierender Schlagvorrichtung zum Zerstören des Deckels
DE3003004C2 (de) * 1980-01-29 1982-06-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Deckel aus leicht zerstörbarem Material zum Verschließen der in die Brennkammer von kombinierten Staustrahl-Raketentriebwerken einmündenden Lufteinlauföffnungen, und Schlagvorrichtung zum Zerstören des Deckels
JPS57131846A (en) * 1981-02-06 1982-08-14 Nissan Motor Co Ltd Ram rocket
US4332631A (en) * 1982-03-04 1982-06-01 Hercules Incorporated Castable silicone based magnesium fueled propellant
FR2549146B1 (fr) * 1983-07-11 1987-12-24 Europ Propulsion Ensemble propulsif pour missile statoreacteur a propulseur d'acceleration integre
DE3407901A1 (de) * 1984-03-03 1985-09-05 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Kombinierte schubduese fuer rueckstosstriebwerke, insbesondere raketen-staubstrahltriebwerke
FR2606082B1 (fr) * 1986-11-05 1991-04-05 Europ Propulsion Chambre de combustion de propulseur a propergol solide, et procede pour sa fabrication
FR2631387B1 (fr) * 1988-05-10 1990-07-13 Poudres & Explosifs Ste Nale Propulseur sans tuyere de faible allongement

Also Published As

Publication number Publication date
GB2411438A (en) 2005-08-31
GB2411438B (en) 2006-03-01
GB8922949D0 (en) 2005-06-08
US8079308B1 (en) 2011-12-20
SE8903302D0 (sv) 1989-10-09
DE3934071B3 (de) 2006-02-23
FR2863665A1 (fr) 2005-06-17
CA1341492C (fr) 2006-01-03

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse

Effective date: 20080630