FR2526086B3 - - Google Patents

Info

Publication number
FR2526086B3
FR2526086B3 FR8112435A FR8112435A FR2526086B3 FR 2526086 B3 FR2526086 B3 FR 2526086B3 FR 8112435 A FR8112435 A FR 8112435A FR 8112435 A FR8112435 A FR 8112435A FR 2526086 B3 FR2526086 B3 FR 2526086B3
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.)
Expired
Application number
FR8112435A
Other languages
French (fr)
Other versions
FR2526086A1 (fr
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 FR2526086A1 publication Critical patent/FR2526086A1/fr
Application granted granted Critical
Publication of FR2526086B3 publication Critical patent/FR2526086B3/fr
Granted 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR8112435A 1980-06-25 1981-06-24 Dispositif pour l'introduction de gaz riches en combustible dans la chambre de combustion de statoreacteurs a fusee Granted FR2526086A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3023755A DE3023755C2 (de) 1980-06-25 1980-06-25 Einrichtung zum Einbringen brennstoffreicher Gase in die Brennkammer von Raketen-Staustrahltriebwerken

Publications (2)

Publication Number Publication Date
FR2526086A1 FR2526086A1 (fr) 1983-11-04
FR2526086B3 true FR2526086B3 (cs) 1984-11-16

Family

ID=6105424

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8112435A Granted FR2526086A1 (fr) 1980-06-25 1981-06-24 Dispositif pour l'introduction de gaz riches en combustible dans la chambre de combustion de statoreacteurs a fusee

Country Status (2)

Country Link
DE (1) DE3023755C2 (cs)
FR (1) FR2526086A1 (cs)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2587414B1 (fr) * 1985-09-17 1987-12-18 Aerospatiale Statoreacteur a guidage du melange air-carburant et missile pourvu d'un tel statoreacteur
DE4437524C2 (de) * 1994-10-20 1997-04-24 Kunkel Klaus Dr Ing Verfahren zum Betreiben eines nach dem Rückstoßprinzip arbeitenden Antriebes eines Flugkörpers sowie Flugkörperantrieb

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2861420A (en) * 1953-03-20 1958-11-25 United Aircraft Corp Fuel regulator
US2927427A (en) * 1955-05-10 1960-03-08 Onera (Off Nat Aerospatiale) Continuous flow thermal machines and in particular in ram-jets and turbojets
US2987875A (en) * 1955-05-26 1961-06-13 Phillips Petroleum Co Ramjet power plants for missiles
US3336753A (en) * 1961-10-06 1967-08-22 Texaco Experiment Inc Propulsion devices
FR2257789A1 (en) * 1973-07-27 1975-08-08 Onera (Off Nat Aerospatiale) Propulsive unit for missile - has jet and rocket with coaxial discharges axially displaced from each other

Also Published As

Publication number Publication date
FR2526086A1 (fr) 1983-11-04
DE3023755C2 (de) 1986-04-03
DE3023755A1 (de) 1983-11-03

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