FR2266806A1 - Series jet rocket engine has two pref parallel shafts - each with one turbine to give reduced shaft and engine length - Google Patents

Series jet rocket engine has two pref parallel shafts - each with one turbine to give reduced shaft and engine length

Info

Publication number
FR2266806A1
FR2266806A1 FR7508423A FR7508423A FR2266806A1 FR 2266806 A1 FR2266806 A1 FR 2266806A1 FR 7508423 A FR7508423 A FR 7508423A FR 7508423 A FR7508423 A FR 7508423A FR 2266806 A1 FR2266806 A1 FR 2266806A1
Authority
FR
France
Prior art keywords
series
turbine
combustion chamber
engine
pref
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.)
Granted
Application number
FR7508423A
Other languages
English (en)
French (fr)
Other versions
FR2266806B1 (de
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 FR2266806A1 publication Critical patent/FR2266806A1/fr
Application granted granted Critical
Publication of FR2266806B1 publication Critical patent/FR2266806B1/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
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7508423A 1974-04-05 1975-03-18 Series jet rocket engine has two pref parallel shafts - each with one turbine to give reduced shaft and engine length Granted FR2266806A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742416766 DE2416766C3 (de) 1974-04-05 1974-04-05 Hauptstromraketentriebwerk

Publications (2)

Publication Number Publication Date
FR2266806A1 true FR2266806A1 (en) 1975-10-31
FR2266806B1 FR2266806B1 (de) 1978-12-29

Family

ID=5912297

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7508423A Granted FR2266806A1 (en) 1974-04-05 1975-03-18 Series jet rocket engine has two pref parallel shafts - each with one turbine to give reduced shaft and engine length

Country Status (4)

Country Link
JP (1) JPS5824616B2 (de)
DE (1) DE2416766C3 (de)
FR (1) FR2266806A1 (de)
IN (1) IN142773B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3003904A1 (fr) * 2013-03-29 2014-10-03 Snecma Moteur de propulsion avec generateur de gaz annulaire

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6065879A (ja) * 1983-09-22 1985-04-15 三洋電機株式会社 自動閉扉装置
FR2921979B1 (fr) * 2007-10-08 2014-06-13 Astrium Sas Dispositif et procede de motorisation de pompe pour moteur fusee par moteur a combustion interne

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977815C (de) * 1963-12-21 1970-12-03 Messerschmitt Boelkow Blohm Fluessigkeitsraketentriebwerk
DE1264870B (de) * 1965-10-21 1968-03-28 Boelkow Gmbh Fluessigkeitsraketentriebwerk

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3003904A1 (fr) * 2013-03-29 2014-10-03 Snecma Moteur de propulsion avec generateur de gaz annulaire

Also Published As

Publication number Publication date
DE2416766A1 (de) 1975-10-16
DE2416766B2 (de) 1977-09-29
JPS50136509A (de) 1975-10-29
DE2416766C3 (de) 1978-05-24
JPS5824616B2 (ja) 1983-05-23
FR2266806B1 (de) 1978-12-29
IN142773B (de) 1977-08-27

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Legal Events

Date Code Title Description
ST Notification of lapse