GB1313322A - Combustion chamber and thrust nozzle - Google Patents

Combustion chamber and thrust nozzle

Info

Publication number
GB1313322A
GB1313322A GB3761070A GB3761070A GB1313322A GB 1313322 A GB1313322 A GB 1313322A GB 3761070 A GB3761070 A GB 3761070A GB 3761070 A GB3761070 A GB 3761070A GB 1313322 A GB1313322 A GB 1313322A
Authority
GB
United Kingdom
Prior art keywords
tubes
spaces
nozzle
length
combustion chamber
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
Application number
GB3761070A
Other languages
English (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 GB1313322A publication Critical patent/GB1313322A/en
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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
GB3761070A 1969-08-14 1970-08-04 Combustion chamber and thrust nozzle Expired GB1313322A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691941297 DE1941297B2 (de) 1969-08-14 1969-08-14 Regenerativ gekuehlte brennkammer und oder schubduese

Publications (1)

Publication Number Publication Date
GB1313322A true GB1313322A (en) 1973-04-11

Family

ID=5742730

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3761070A Expired GB1313322A (en) 1969-08-14 1970-08-04 Combustion chamber and thrust nozzle

Country Status (3)

Country Link
DE (1) DE1941297B2 (enrdf_load_stackoverflow)
FR (1) FR2058270B1 (enrdf_load_stackoverflow)
GB (1) GB1313322A (enrdf_load_stackoverflow)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109884243A (zh) * 2018-12-21 2019-06-14 西安航天动力研究所 一种带主动冷却大热流超声速射流喷管

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2977754A (en) * 1958-01-29 1961-04-04 Thiokol Chemical Corp Rocket chamber with multi-pass axial flow coolant passageways
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
US3460759A (en) * 1967-03-07 1969-08-12 Nasa Combustion chamber

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109884243A (zh) * 2018-12-21 2019-06-14 西安航天动力研究所 一种带主动冷却大热流超声速射流喷管
CN109884243B (zh) * 2018-12-21 2023-12-26 西安航天动力研究所 一种带主动冷却大热流超声速射流喷管

Also Published As

Publication number Publication date
DE1941297A1 (de) 1971-03-11
FR2058270A1 (enrdf_load_stackoverflow) 1971-05-28
DE1941297B2 (de) 1971-11-18
FR2058270B1 (enrdf_load_stackoverflow) 1975-02-21

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee