GB9012648D0 - Combination propulsion means for hypersonic flight - Google Patents

Combination propulsion means for hypersonic flight

Info

Publication number
GB9012648D0
GB9012648D0 GB909012648A GB9012648A GB9012648D0 GB 9012648 D0 GB9012648 D0 GB 9012648D0 GB 909012648 A GB909012648 A GB 909012648A GB 9012648 A GB9012648 A GB 9012648A GB 9012648 D0 GB9012648 D0 GB 9012648D0
Authority
GB
United Kingdom
Prior art keywords
propulsion means
hypersonic flight
combination propulsion
combination
hypersonic
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.)
Withdrawn
Application number
GB909012648A
Other versions
GB2235249A (en
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 GB9012648D0 publication Critical patent/GB9012648D0/en
Publication of GB2235249A publication Critical patent/GB2235249A/en
Withdrawn legal-status Critical Current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
    • F02K7/16—Composite ram-jet/turbo-jet 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)
GB9012648A 1989-07-05 1990-06-06 Propulsion means for hypersonic flight Withdrawn GB2235249A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3922018A DE3922018A1 (en) 1989-07-05 1989-07-05 HYPERSONIC COMBINATION DRIVE

Publications (2)

Publication Number Publication Date
GB9012648D0 true GB9012648D0 (en) 1990-07-25
GB2235249A GB2235249A (en) 1991-02-27

Family

ID=6384298

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9012648A Withdrawn GB2235249A (en) 1989-07-05 1990-06-06 Propulsion means for hypersonic flight

Country Status (3)

Country Link
DE (1) DE3922018A1 (en)
FR (1) FR2649446A1 (en)
GB (1) GB2235249A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7305816B2 (en) 2004-08-13 2007-12-11 United Technologies Corporation Rocket augmentation for combined cycle turboaccelerator jet engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003004C2 (en) * 1980-01-29 1982-06-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Lid made of easily destructible material for closing the air inlet openings that open into the combustion chamber of combined ramjet rocket engines, and striking device for destroying the lid
US4381642A (en) * 1980-06-20 1983-05-03 The Boeing Company Ramjet engine
GB2165338B (en) * 1984-10-06 1988-11-02 Rolls Royce Integral rocket and ramjet engine
DE3811614C1 (en) * 1988-04-07 1989-05-18 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De

Also Published As

Publication number Publication date
DE3922018A1 (en) 1991-01-17
GB2235249A (en) 1991-02-27
DE3922018C2 (en) 1991-12-12
FR2649446A1 (en) 1991-01-11

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)