[go: up one dir, main page]

FR1229596A - Moteur-fusée - Google Patents

Moteur-fusée

Info

Publication number
FR1229596A
FR1229596A FR800085A FR800085A FR1229596A FR 1229596 A FR1229596 A FR 1229596A FR 800085 A FR800085 A FR 800085A FR 800085 A FR800085 A FR 800085A FR 1229596 A FR1229596 A FR 1229596A
Authority
FR
France
Prior art keywords
rocket engine
rocket
engine
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
FR800085A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of FR1229596A publication Critical patent/FR1229596A/fr
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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/128—Nozzles
    • F05D2240/1281—Plug nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
FR800085A 1958-07-21 1959-07-15 Moteur-fusée Expired FR1229596A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US749744A US3112612A (en) 1958-07-21 1958-07-21 Rocket motor

Publications (1)

Publication Number Publication Date
FR1229596A true FR1229596A (fr) 1960-09-08

Family

ID=25014997

Family Applications (1)

Application Number Title Priority Date Filing Date
FR800085A Expired FR1229596A (fr) 1958-07-21 1959-07-15 Moteur-fusée

Country Status (3)

Country Link
US (1) US3112612A (fr)
DE (1) DE1115080B (fr)
FR (1) FR1229596A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3107488A (en) * 1960-09-27 1963-10-22 Astrosyst Inc Rotating rocket motor
US3151453A (en) * 1961-05-09 1964-10-06 Rolls Royce Reheat combustion apparatus for a gas turbine engine
US3279183A (en) * 1962-09-07 1966-10-18 United Aircraft Corp Vectorable plug cluster nozzle rocket
US3312068A (en) * 1960-12-05 1967-04-04 North American Aviation Inc Horizontal flow thrust chamber
US3314609A (en) * 1962-09-07 1967-04-18 United Aircraft Corp Vectorable plug cluster nozzle rocket

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3270501A (en) * 1964-03-05 1966-09-06 James E Webb Aerodynamic spike nozzle
DE1297942B (de) * 1966-11-29 1969-06-19 Kayser Lutz T Anordnung zur Raketentriebwerkskuehlung
DE1809348A1 (de) * 1968-11-16 1970-06-25 Messerschmitt Boelkow Blohm Gasgenerator (Brennkammer),insbesondere Vorbrennkammer fuer ein Raketentriebwerk in Hauptstrombauart
JPS5256209A (en) * 1976-01-07 1977-05-09 Hitoshi Kukitsu Liquid fuel rocket of air absorbing type
US5129604A (en) * 1989-07-17 1992-07-14 General Dynamics Corporation, Pomona Div. Lateral thrust assembly for missiles
US6516605B1 (en) * 2001-06-15 2003-02-11 General Electric Company Pulse detonation aerospike engine
US7849695B1 (en) 2001-09-17 2010-12-14 Alliant Techsystems Inc. Rocket thruster comprising load-balanced pintle valve
US6655124B2 (en) * 2002-02-26 2003-12-02 Northrop Grumman Corporation External system and method for rocket exhaust plume signature tailoring
US6629416B1 (en) * 2002-04-25 2003-10-07 The United States Of America As Represented By The Secretary Of The Navy Afterburning aerospike rocket nozzle
US6964154B1 (en) * 2003-03-11 2005-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Axisymmetric, throttleable non-gimballed rocket engine
US7565797B2 (en) * 2004-02-27 2009-07-28 Ghkn Engineering Llc Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles
US20050210862A1 (en) * 2004-03-25 2005-09-29 Paterro Von Friedrich C Quantum jet turbine propulsion system
US20090211225A1 (en) * 2007-01-29 2009-08-27 Ghkn Engineering, Llc Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles
FR2924763B1 (fr) * 2007-12-06 2014-04-25 Snecma Systeme de tuyeres de moteur-fusee
CN101718236A (zh) * 2010-02-10 2010-06-02 周林 有爆震转射器连通的多管脉冲爆震燃烧室
US10920714B2 (en) * 2013-03-15 2021-02-16 Exquadrum, Inc. Stable hybrid rocket technology
EP4114739A4 (fr) * 2020-05-08 2024-04-10 Orbion Space Technology, Inc. Système de propulsion pour engin spatial
US11512669B2 (en) * 2020-06-24 2022-11-29 Raytheon Company Distributed airfoil aerospike rocket nozzle
US11933249B2 (en) * 2021-12-30 2024-03-19 Blue Origin, Llc Reusable upper stage rocket with aerospike engine
CN118423565B (zh) * 2024-07-03 2024-11-26 西安航天动力研究所 一种火箭发动机的传力架

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2396567A (en) * 1940-11-19 1946-03-12 Daniel And Florence Guggenheim Combustion apparatus
US2601194A (en) * 1941-12-01 1952-06-17 Power Jets Res & Dev Ltd Multiunit gas turbine power plant for aircraft propulsion
GB633336A (en) * 1944-08-26 1949-12-12 Claude Albert Bonvillian Apparatus for the combustion of combustible and vaporizable substances
CH253328A (de) * 1945-06-27 1948-02-29 Ljungstrom Birger Kraftanlage.
US2714999A (en) * 1949-04-20 1955-08-09 Fairchild Engine & Airplane Jet propelled bombing aircraft
FR1012021A (fr) * 1949-05-19 1952-07-02 Soc Tech De Rech Ind Perfectionnements aux réacteurs
BE498317A (fr) * 1949-10-06
US2753687A (en) * 1950-10-02 1956-07-10 Gen Electric Injection head for jet propulsion system
FR1036205A (fr) * 1951-04-26 1953-09-04 Perfectionnements apportés aux projectiles auto-propulsés à charge explosive, notamment aux obus explosifs auto-propulsés
US2703962A (en) * 1952-09-30 1955-03-15 Delwyn L Olson Rocket engine injector head
GB749009A (en) * 1953-04-24 1956-05-16 Power Jets Res & Dev Ltd An improved jet propulsion plant
BE537645A (fr) * 1954-06-10

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3107488A (en) * 1960-09-27 1963-10-22 Astrosyst Inc Rotating rocket motor
US3312068A (en) * 1960-12-05 1967-04-04 North American Aviation Inc Horizontal flow thrust chamber
US3151453A (en) * 1961-05-09 1964-10-06 Rolls Royce Reheat combustion apparatus for a gas turbine engine
US3279183A (en) * 1962-09-07 1966-10-18 United Aircraft Corp Vectorable plug cluster nozzle rocket
US3314609A (en) * 1962-09-07 1967-04-18 United Aircraft Corp Vectorable plug cluster nozzle rocket

Also Published As

Publication number Publication date
US3112612A (en) 1963-12-03
DE1115080B (de) 1961-10-12

Similar Documents

Publication Publication Date Title
FR1229596A (fr) Moteur-fusée
FR1239933A (fr) Explosifs
CH374857A (de) Brennkammer
FR1203995A (fr) Moteur-fusée perfectionné
BE617315A (fr) Moteur-fusée
CH381019A (de) Mehrfachtriebwerk
CH367054A (de) Schubumkehrvorrichtung
CH400673A (de) Raketenmotor
CH369984A (de) Raketenmotor mit Leuchtsatz
FR1201360A (fr) Moteur fusée
CH396513A (de) Treibstoff
FR1218345A (fr) Projectile
CH388014A (de) Kraftstoff
FR1230372A (fr) Moteur-fusée
FR1227109A (fr) Fusée de projectile
FR1191494A (fr) Perfectionnements aux roquettes
CH377378A (de) Turbine
AT207174B (de) Kolbenmaschine
CH411743A (de) Sprengstoffbetätigtes Treibwerk
CH367009A (de) Raketenmotor
BE582754A (fr) Détonateurs
CH368341A (de) Brennstoffpumpe
FR1256441A (fr) Perfectionnements à des moteurs de fusée
FR1239553A (fr) Moteurs de fusées
BE590729A (fr) Perfectionnements aux moteurs-fusée