FR2626317B1 - Groupe de fond pour la chambre de combustion d'une fusee a liquides - Google Patents

Groupe de fond pour la chambre de combustion d'une fusee a liquides

Info

Publication number
FR2626317B1
FR2626317B1 FR898900149A FR8900149A FR2626317B1 FR 2626317 B1 FR2626317 B1 FR 2626317B1 FR 898900149 A FR898900149 A FR 898900149A FR 8900149 A FR8900149 A FR 8900149A FR 2626317 B1 FR2626317 B1 FR 2626317B1
Authority
FR
France
Prior art keywords
combustion chamber
liquid rocket
bottom group
group
rocket
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 - Fee Related
Application number
FR898900149A
Other languages
English (en)
French (fr)
Other versions
FR2626317A1 (fr
Inventor
Thomas Barth
Heinz Keller
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.)
Carl Freudenberg KG
Original Assignee
Carl Freudenberg KG
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 Carl Freudenberg KG filed Critical Carl Freudenberg KG
Publication of FR2626317A1 publication Critical patent/FR2626317A1/fr
Application granted granted Critical
Publication of FR2626317B1 publication Critical patent/FR2626317B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/52—Injectors
    • 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
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L27/00—Adjustable joints; Joints allowing movement
    • F16L27/10—Adjustable joints; Joints allowing movement comprising a flexible connection only
    • F16L27/103—Adjustable joints; Joints allowing movement comprising a flexible connection only in which a flexible element, e.g. a rubber-metal laminate, which undergoes constraints consisting of shear and flexure, is sandwiched between partly curved surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Support Of The Bearing (AREA)
  • Toys (AREA)
FR898900149A 1988-01-27 1989-01-09 Groupe de fond pour la chambre de combustion d'une fusee a liquides Expired - Fee Related FR2626317B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3802257A DE3802257C1 (https=) 1988-01-27 1988-01-27

Publications (2)

Publication Number Publication Date
FR2626317A1 FR2626317A1 (fr) 1989-07-28
FR2626317B1 true FR2626317B1 (fr) 1994-06-17

Family

ID=6346025

Family Applications (1)

Application Number Title Priority Date Filing Date
FR898900149A Expired - Fee Related FR2626317B1 (fr) 1988-01-27 1989-01-09 Groupe de fond pour la chambre de combustion d'une fusee a liquides

Country Status (3)

Country Link
US (1) US4901526A (https=)
DE (1) DE3802257C1 (https=)
FR (1) FR2626317B1 (https=)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2126905C1 (ru) * 1998-03-12 1999-02-27 Федеральное государственное унитарное предприятие "Исследовательский центр им.М.В.Келдыша" Камера сгорания
US6138451A (en) * 1998-05-11 2000-10-31 Hughes Electronics Corporation Rocket engine with combustion chamber step structure insert, and its fabrication
WO2011106446A1 (en) * 2010-02-24 2011-09-01 Innovative Defense, Llc Packaged propellant air-induced variable thrust rocket engine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049877A (en) * 1956-02-13 1962-08-21 Thiokol Chemical Corp Nozzle for reaction motor
US3140584A (en) * 1959-05-07 1964-07-14 Thiokol Chemical Corp Steering device for rocket-powered vehicles
US3016697A (en) * 1959-06-19 1962-01-16 Curtiss Wright Corp Rocket engine swivel mount
US3138922A (en) * 1962-01-22 1964-06-30 Buehler Corp Rotating conduit control
FR1332562A (fr) * 1962-03-20 1963-07-19 Snecma Dispositif de tourillonnement et d'étanchéité pour tuyère, applicable notamment aux fusées
US3145530A (en) * 1962-09-27 1964-08-25 Gen Motors Corp Multistage rocket
US3280563A (en) * 1962-10-26 1966-10-25 Charles F Bowersett Thrust vectoring system
US3659423A (en) * 1964-09-17 1972-05-02 Goodyear Aerospace Corp Moveable rocket
GB1189052A (en) * 1968-01-09 1970-04-22 Lockheed Aircraft Corp Flexible Joint Means
FR2034339B1 (https=) * 1969-03-18 1974-12-06 Bringer Henri
US3958840A (en) * 1975-05-05 1976-05-25 Thiokol Corporation Flexible bearing having reinforcements
US3941433A (en) * 1975-05-05 1976-03-02 Thiokol Corporation Flexible bearing having low torque resistance
US4103939A (en) * 1976-06-15 1978-08-01 Murdock Machine & Engineering Company Multi passage flexible connector

Also Published As

Publication number Publication date
US4901526A (en) 1990-02-20
DE3802257C1 (https=) 1989-07-20
FR2626317A1 (fr) 1989-07-28

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Legal Events

Date Code Title Description
ST Notification of lapse