FR2693235B1 - Tuyère et moteur-fusée pour leurre. - Google Patents

Tuyère et moteur-fusée pour leurre.

Info

Publication number
FR2693235B1
FR2693235B1 FR9307991A FR9307991A FR2693235B1 FR 2693235 B1 FR2693235 B1 FR 2693235B1 FR 9307991 A FR9307991 A FR 9307991A FR 9307991 A FR9307991 A FR 9307991A FR 2693235 B1 FR2693235 B1 FR 2693235B1
Authority
FR
France
Prior art keywords
lure
nozzle
rocket motor
rocket
motor
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
FR9307991A
Other languages
English (en)
Other versions
FR2693235A1 (fr
Inventor
Robert Brogan
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.)
Aerojet Rocketdyne Inc
Original Assignee
Aerojet General Corp
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 Aerojet General Corp filed Critical Aerojet General Corp
Publication of FR2693235A1 publication Critical patent/FR2693235A1/fr
Application granted granted Critical
Publication of FR2693235B1 publication Critical patent/FR2693235B1/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
    • F02K9/97—Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Testing Of Engines (AREA)
FR9307991A 1992-07-01 1993-06-30 Tuyère et moteur-fusée pour leurre. Expired - Fee Related FR2693235B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/907,466 US5251436A (en) 1992-07-01 1992-07-01 Thrust-reducing, chaotic-flow nozzle

Publications (2)

Publication Number Publication Date
FR2693235A1 FR2693235A1 (fr) 1994-01-07
FR2693235B1 true FR2693235B1 (fr) 1994-10-28

Family

ID=25424143

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9307991A Expired - Fee Related FR2693235B1 (fr) 1992-07-01 1993-06-30 Tuyère et moteur-fusée pour leurre.

Country Status (4)

Country Link
US (1) US5251436A (fr)
JP (1) JPH06105067B2 (fr)
DE (1) DE4321806C2 (fr)
FR (1) FR2693235B1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2733315B1 (fr) * 1995-04-10 1997-06-13 Hamy Gerard Moteur-pousseur pour projectiles sans etuis tous calibres
US6199768B1 (en) 1999-03-18 2001-03-13 Exxon Research And Engineering Company Process and apparatus for atomizing FCC feed oil
US6783662B2 (en) 1999-03-18 2004-08-31 Exxonmobil Research And Engineering Company Cavitation enhanced liquid atomization
AU6795200A (en) 1999-08-26 2001-03-19 Exxonmobil Research And Engineering Company Superheating atomizing steam with hot fcc feed oil
US6224434B1 (en) 1999-09-07 2001-05-01 Bombardier Motor Corporation Of America Pump jet with axial directional flow control device for thrust modulation
US6430920B1 (en) 1999-11-23 2002-08-13 Technanogy, Llc Nozzleless rocket motor
US6796704B1 (en) * 2000-06-06 2004-09-28 W. Gerald Lott Apparatus and method for mixing components with a venturi arrangement
US6684622B2 (en) 2002-02-26 2004-02-03 Northrop Grumman Corporation Rocket exhaust plume signature tailoring
US6655124B2 (en) 2002-02-26 2003-12-02 Northrop Grumman Corporation External system and method for rocket exhaust plume signature tailoring
US7377217B2 (en) * 2004-10-18 2008-05-27 The Boeing Company Decoy device and system for anti-missile protection and associated method
US20100024388A1 (en) * 2007-11-02 2010-02-04 Korea Aerospace Research Institute Flow-Restricting Filter, Solid Propellant Gas Generator and Propulsion System Comprising the Same
KR100988260B1 (ko) * 2008-05-23 2010-10-18 한국항공우주연구원 분사 노즐 조립체 및 이를 포함하는 고체 추진제 가스발생기
CN107942292A (zh) * 2017-10-27 2018-04-20 四川嘉义雷科电子技术有限公司 设置有气体冷却装置的测距设备

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE564936C (de) * 1929-03-04 1932-11-24 Ceskoslovenske Municni A Kovod Leuchtspur- oder Brandgeschoss
DE729133C (de) * 1939-05-12 1942-12-10 Bohdan Pantoflicek Verschluss von Treibfuellungen von Minen, Geschossen, Granaten u. aehnl.
FR989809A (fr) * 1949-04-29 1951-09-13 S E R A M Soc D Etudes Perfectionnement aux fusées
US3012400A (en) * 1960-05-23 1961-12-12 Jr Blake W Corson Nozzle
US3208384A (en) * 1964-01-21 1965-09-28 Fountain Gilbert Rocket thrust neutralizer
US3341129A (en) * 1964-07-13 1967-09-12 Atlantic Res Corp Rocket nozzle
US3344603A (en) * 1965-07-28 1967-10-03 United Aircraft Corp Variable impulse rocket motor
US3691770A (en) * 1966-12-02 1972-09-19 Us Navy Thrust control means for a solid propellant rocket motor
US3453958A (en) * 1968-02-20 1969-07-08 William Lai Infrared flare having a shroud for enhancing the radiation thereof
US3938444A (en) * 1974-07-05 1976-02-17 The United States Of America As Represented By The Secretary Of The Navy Flare cartridge
US4011720A (en) * 1975-05-13 1977-03-15 Thiokol Corporation Gas generator or rocket motor with selective discrete time vs. output profiles
GB2014664B (en) * 1978-02-15 1982-07-14 Secr Defence Shock wave attenuators
DE3246380A1 (de) * 1982-12-15 1984-06-20 Diehl GmbH & Co, 8500 Nürnberg Vorrichtung zur reduzierung des bodenwiderstandes bei geschossen
US4452039A (en) * 1983-07-06 1984-06-05 The United States Of America As Represented By The Secretary Of The Navy Expendable infrared source and method therefor
FR2549146B1 (fr) * 1983-07-11 1987-12-24 Europ Propulsion Ensemble propulsif pour missile statoreacteur a propulseur d'acceleration integre
DE3507892A1 (de) * 1985-03-06 1986-09-11 Rheinmetall GmbH, 4000 Düsseldorf Gasgenerator
CA1265988A (fr) * 1986-05-26 1990-02-20 John Louis Halpin Dispositif d'entretien des flammes de carburants a teneur de pyrophore dans l'air a tres haute velocite

Also Published As

Publication number Publication date
US5251436A (en) 1993-10-12
JPH0658204A (ja) 1994-03-01
FR2693235A1 (fr) 1994-01-07
JPH06105067B2 (ja) 1994-12-21
DE4321806A1 (de) 1994-01-05
DE4321806C2 (de) 1995-06-01

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Legal Events

Date Code Title Description
ST Notification of lapse