IT1194031B - Dispositivo ugello/valvola per motore a razzo intubato - Google Patents

Dispositivo ugello/valvola per motore a razzo intubato

Info

Publication number
IT1194031B
IT1194031B IT20262/81A IT2026281A IT1194031B IT 1194031 B IT1194031 B IT 1194031B IT 20262/81 A IT20262/81 A IT 20262/81A IT 2026281 A IT2026281 A IT 2026281A IT 1194031 B IT1194031 B IT 1194031B
Authority
IT
Italy
Prior art keywords
intubated
nozzle
valve device
rocket motor
rocket
Prior art date
Application number
IT20262/81A
Other languages
English (en)
Other versions
IT8120262A0 (it
Inventor
William Marion Burkes
William Hamilton Miller
Original Assignee
Hercules Inc
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 Hercules Inc filed Critical Hercules Inc
Publication of IT8120262A0 publication Critical patent/IT8120262A0/it
Application granted granted Critical
Publication of IT1194031B publication Critical patent/IT1194031B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lift Valve (AREA)
  • Fuel-Injection Apparatus (AREA)
IT20262/81A 1980-03-11 1981-03-10 Dispositivo ugello/valvola per motore a razzo intubato IT1194031B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/129,284 US4355663A (en) 1980-03-11 1980-03-11 Nozzle/valve device for a ducted rocket motor

Publications (2)

Publication Number Publication Date
IT8120262A0 IT8120262A0 (it) 1981-03-10
IT1194031B true IT1194031B (it) 1988-08-31

Family

ID=22439281

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20262/81A IT1194031B (it) 1980-03-11 1981-03-10 Dispositivo ugello/valvola per motore a razzo intubato

Country Status (6)

Country Link
US (1) US4355663A (it)
CA (1) CA1166855A (it)
DE (1) DE3109269A1 (it)
FR (1) FR2482328B1 (it)
GB (1) GB2071285B (it)
IT (1) IT1194031B (it)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4444006A (en) * 1981-02-04 1984-04-24 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
US4442669A (en) * 1981-02-12 1984-04-17 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
US4416112A (en) * 1981-12-28 1983-11-22 Hercules Incorporated Fuel injector for ducted rocket motor
US4574586A (en) * 1984-02-16 1986-03-11 Hercules Incorporated Self compensating ducted rocket motor fuel nozzle and method for regulating fuel generation
DE3507892A1 (de) * 1985-03-06 1986-09-11 Rheinmetall GmbH, 4000 Düsseldorf Gasgenerator
DE3531189A1 (de) * 1985-08-31 1987-03-12 Rheinmetall Gmbh Ventilanordnung
FR2588372B1 (fr) * 1985-10-08 1989-07-13 Thomson Brandt Armements Dispositif de pilotage pour projectile guide au moyen de tuyeres laterales
US4817377A (en) * 1987-05-07 1989-04-04 Morton Thiokol, Inc. Head end control and steering system: using a forward end maneuvering gas generator
US5817968A (en) * 1987-08-03 1998-10-06 The United States Of America As Represented By The Secretary Of The Air Force Gas generation with high pressure sensitivity exponent propellant
US5172547A (en) * 1991-04-30 1992-12-22 The United States Of America As Represented By The Secretary Of The Air Force Electronic valve control for gas generator outflow
US5341639A (en) * 1993-01-19 1994-08-30 The United States Of America As Represented By The Secretary Of The Army Fullerene rocket fuels
DE19924907B4 (de) * 1999-05-31 2007-06-28 Eads Space Transportation Gmbh Feststofftriebwerk für eine Staustrahlrakete
CN104929810A (zh) * 2014-03-17 2015-09-23 南京理工大学 直线电机驱动的固体火箭冲压发动机燃气流量调节装置
FR3021363B1 (fr) * 2014-05-21 2019-05-03 Safran Aircraft Engines Dispositif de regulation de debit ameliore ayant une masse reduite
US10072613B2 (en) 2015-02-23 2018-09-11 Orbital Atk, Inc. Methods of forming flexible structures for a rocket motor assembly, related flexible structures, and related assemblies including the flexible structures
US20170096962A1 (en) * 2015-07-13 2017-04-06 Aerojet Rocketdyne, Inc. Throat area control system
KR101986499B1 (ko) * 2018-12-10 2019-06-07 엘아이지넥스원 주식회사 고온 가스 유량 조절용 가스 발생기
RU2736089C1 (ru) * 2020-06-18 2020-11-11 Акционерное общество "Машиностроительное конструкторское бюро "Искра" имени Ивана Ивановича Картукова" (АО "МКБ "Искра") Двухрежимный сопловой блок

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1946319A (en) * 1931-11-05 1934-02-06 Kent Ltd G Variable orifice for measuring the flow of fluids
US2889117A (en) * 1955-05-13 1959-06-02 Garrett Corp Turbine speed control
US2968919A (en) * 1957-03-25 1961-01-24 Hughes Aircraft Co Variable area nozzle
FR1309582A (fr) * 1961-04-01 1962-11-16 Huettenwerk Oberhausen Ag Dispositif de fermeture pour poches de coulée et mode d'utilisation
US3192709A (en) * 1962-10-17 1965-07-06 Hardy Sammie Lloyd Variable throat nozzle
US3332237A (en) * 1964-10-27 1967-07-25 Fiego Louis Lo Mechanical valve
US3524473A (en) * 1968-01-11 1970-08-18 Moog Inc Flow control valve having constant outlet orifice area
US3760589A (en) * 1969-03-24 1973-09-25 Thiokol Chemical Corp Throttling mechanism for controlling the thrust level of a solid propellant rocket motor
US3780982A (en) * 1972-12-08 1973-12-25 Acf Ind Inc Control ports for gate valve structure
DE2943891C2 (de) * 1979-10-31 1982-09-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Betätigungsvorrichtung für ein Ventil zum Verändern des Durchströmquerschnitts einer Heißgasleitung, insbesondere für in die Brennkammer von Staustrahltriebwerken einströmende brennstoffreiche Gase

Also Published As

Publication number Publication date
DE3109269C2 (it) 1991-12-12
US4355663A (en) 1982-10-26
GB2071285B (en) 1983-04-13
FR2482328B1 (fr) 1985-06-21
FR2482328A1 (fr) 1981-11-13
IT8120262A0 (it) 1981-03-10
DE3109269A1 (de) 1982-02-25
CA1166855A (en) 1984-05-08
GB2071285A (en) 1981-09-16

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