DE1626061B1 - Mehrteilige Raketenbrennkammer mit Schubdüse - Google Patents

Mehrteilige Raketenbrennkammer mit Schubdüse

Info

Publication number
DE1626061B1
DE1626061B1 DE19671626061 DE1626061A DE1626061B1 DE 1626061 B1 DE1626061 B1 DE 1626061B1 DE 19671626061 DE19671626061 DE 19671626061 DE 1626061 A DE1626061 A DE 1626061A DE 1626061 B1 DE1626061 B1 DE 1626061B1
Authority
DE
Germany
Prior art keywords
combustion chamber
thrust nozzle
nozzle
thrust
piston
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.)
Pending
Application number
DE19671626061
Other languages
German (de)
English (en)
Inventor
Karl Butter
Karl Dipl-Ing Stoeckl
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 DE1626061B1 publication Critical patent/DE1626061B1/de
Pending 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
DE19671626061 1967-07-13 1967-07-13 Mehrteilige Raketenbrennkammer mit Schubdüse Pending DE1626061B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB0093463 1967-07-13

Publications (1)

Publication Number Publication Date
DE1626061B1 true DE1626061B1 (de) 1971-03-04

Family

ID=6986982

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19671626061 Pending DE1626061B1 (de) 1967-07-13 1967-07-13 Mehrteilige Raketenbrennkammer mit Schubdüse

Country Status (4)

Country Link
US (1) US3568929A (enExample)
DE (1) DE1626061B1 (enExample)
FR (1) FR1572019A (enExample)
GB (1) GB1227556A (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5060550A (en) * 1991-02-19 1991-10-29 The United States Of America As Represented By The Secretary Of The Navy Rocket nozzle snubber
US5219190A (en) * 1991-05-13 1993-06-15 General Electric Company Shear wire flange joint for a gas turbine engine
US5224818A (en) * 1991-11-01 1993-07-06 General Electric Company Air transfer bushing
US5560559A (en) * 1994-06-30 1996-10-01 Alliedsignal, Inc. Actuation system with active compensation for transient loads
US5607123A (en) * 1994-06-30 1997-03-04 Alliedsignal Inc. Actuation system with passive compensation for transient loads
US6702300B1 (en) * 2002-01-11 2004-03-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration High temperature seal for large structural movements
GB2385643B (en) * 2002-02-20 2005-05-18 Cross Mfg Company Improvements relating to a fluid seal
FR3042542B1 (fr) * 2015-10-20 2017-12-01 Snecma Chambre propulsive et procede de fabrication

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1135050A (fr) * 1955-10-31 1957-04-23 Soc Tech De Rech Ind Perfectionnements aux dispositifs de sécurité pour propulseurs
DE1235674B (de) * 1962-03-20 1967-03-02 Snecma Duese fuer ein Raketentriebwerk

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2712458A (en) * 1950-06-05 1955-07-05 Lipson Leonard Pipe couplings
US3243124A (en) * 1961-05-01 1966-03-29 Aerojet General Co Nozzle mounting for rocket motor
US3253785A (en) * 1962-09-12 1966-05-31 Kelsey Hayes Co Rocket nozzle construction

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1135050A (fr) * 1955-10-31 1957-04-23 Soc Tech De Rech Ind Perfectionnements aux dispositifs de sécurité pour propulseurs
DE1235674B (de) * 1962-03-20 1967-03-02 Snecma Duese fuer ein Raketentriebwerk

Also Published As

Publication number Publication date
US3568929A (en) 1971-03-09
FR1572019A (enExample) 1969-06-20
GB1227556A (enExample) 1971-04-07

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