IT1196185B - Assieme propulsivo per missile statoreattore a propulsore di accelerazione integrato - Google Patents

Assieme propulsivo per missile statoreattore a propulsore di accelerazione integrato

Info

Publication number
IT1196185B
IT1196185B IT21823/84A IT2182384A IT1196185B IT 1196185 B IT1196185 B IT 1196185B IT 21823/84 A IT21823/84 A IT 21823/84A IT 2182384 A IT2182384 A IT 2182384A IT 1196185 B IT1196185 B IT 1196185B
Authority
IT
Italy
Prior art keywords
propulsor
stator
integrated acceleration
propulsive assembly
missile
Prior art date
Application number
IT21823/84A
Other languages
English (en)
Italian (it)
Other versions
IT8421823A1 (it
IT8421823A0 (it
Inventor
Tanter Gerard Le
Bernard Luscan
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Publication of IT8421823A0 publication Critical patent/IT8421823A0/it
Publication of IT8421823A1 publication Critical patent/IT8421823A1/it
Application granted granted Critical
Publication of IT1196185B publication Critical patent/IT1196185B/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
    • F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section

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)
  • Testing Of Engines (AREA)
  • Stored Programmes (AREA)
  • Earth Drilling (AREA)
IT21823/84A 1983-07-11 1984-07-10 Assieme propulsivo per missile statoreattore a propulsore di accelerazione integrato IT1196185B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8311555A FR2549146B1 (fr) 1983-07-11 1983-07-11 Ensemble propulsif pour missile statoreacteur a propulseur d'acceleration integre

Publications (3)

Publication Number Publication Date
IT8421823A0 IT8421823A0 (it) 1984-07-10
IT8421823A1 IT8421823A1 (it) 1986-01-10
IT1196185B true IT1196185B (it) 1988-11-10

Family

ID=9290725

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21823/84A IT1196185B (it) 1983-07-11 1984-07-10 Assieme propulsivo per missile statoreattore a propulsore di accelerazione integrato

Country Status (6)

Country Link
US (1) US4631916A (cg-RX-API-DMAC7.html)
JP (1) JPS60173352A (cg-RX-API-DMAC7.html)
DE (1) DE3425352C2 (cg-RX-API-DMAC7.html)
FR (1) FR2549146B1 (cg-RX-API-DMAC7.html)
GB (1) GB2143282B (cg-RX-API-DMAC7.html)
IT (1) IT1196185B (cg-RX-API-DMAC7.html)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4817379A (en) * 1985-01-09 1989-04-04 Bagley Charles S Jet propulsion engine and method
US5070691A (en) * 1988-08-03 1991-12-10 Thiokol Corporation Solid propellant canister loaded multiple pulsed or staged rocket
FR2863665B1 (fr) * 1988-10-12 2007-03-30 Aerospatiale Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur
US5251436A (en) * 1992-07-01 1993-10-12 Aerojet General Corporation Thrust-reducing, chaotic-flow nozzle
US6016652A (en) * 1994-10-21 2000-01-25 Hy-Pat Corporation Hybrid rocket system with disposable cartridge
US5831155A (en) * 1996-12-02 1998-11-03 Atlantic Research Corporation Apparatus and method for simulating rocket-to-ramjet transition in a propulsion system
RU2168048C2 (ru) * 1998-10-13 2001-05-27 Тамбовский военный авиационный инженерный институт Ракетно-прямоточный двигатель
US6481198B1 (en) 1999-07-09 2002-11-19 Alliant Techsystems Inc. Multi-stage rocket motor assembly including jettisonable launch motor integrated with flight igniter
RU2175726C1 (ru) * 2000-05-26 2001-11-10 Открытое акционерное общество Научно-производственное объединение "Искра" Твердотопливная разгонная двигательная установка
FR2813344B1 (fr) * 2000-08-28 2002-11-29 Aerospatiale Matra Missiles Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur
RU2211358C1 (ru) * 2002-05-06 2003-08-27 Открытое акционерное общество Научно-производственное объединение "Искра" Разгонная двигательная установка
EP1608863B1 (en) * 2003-03-28 2012-06-20 Mojave Aerospace Ventures, Llc Unitized hybrid rocket system
US7464535B2 (en) * 2004-06-29 2008-12-16 Honeywell International Inc. Rocket motor nozzle throat area control system and method
USD580465S1 (en) * 2007-08-20 2008-11-11 Laurence Waters Warp drive for aerospace vehicle
US8117847B2 (en) * 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
RU2532954C1 (ru) * 2013-04-11 2014-11-20 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Беспилотный летательный аппарат
RU2635758C1 (ru) * 2016-11-14 2017-11-15 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Система регулирования сверхзвукового прямоточного воздушно-реактивного двигателя
CN112682217B (zh) * 2020-12-24 2022-02-15 中国人民解放军国防科技大学 一种基于环形增压中心体后缘扩张火箭冲压宽速域发动机

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510147A (en) * 1945-03-07 1950-06-06 Leslie A Skinner Side venting rocket
US3182447A (en) * 1957-02-27 1965-05-11 Thiokol Chemical Corp Reaction motor
US3094072A (en) * 1957-12-09 1963-06-18 Arthur R Parilla Aircraft, missiles, missile weapons systems, and space ships
US3221497A (en) * 1962-06-29 1965-12-07 Jr Ernest E Forbes Ramjet propulsion system
US3319424A (en) * 1965-09-30 1967-05-16 Frederick L Haake Method and means for supporting a ram-jet propellant
US3807170A (en) * 1967-03-16 1974-04-30 Us Army Fuel injection subsystem for supersonic combustion
US3482403A (en) * 1968-04-08 1969-12-09 Us Navy Corner inlet blowout dome
US4327886A (en) * 1972-11-30 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Integral rocket ramjet missile
FR2257789A1 (en) * 1973-07-27 1975-08-08 Onera (Off Nat Aerospatiale) Propulsive unit for missile - has jet and rocket with coaxial discharges axially displaced from each other
US4109867A (en) * 1977-01-14 1978-08-29 The United States Of America As Represented By The Secretary Of The Navy Two-position nozzle
US4277940A (en) * 1979-07-25 1981-07-14 United Technologies Corporation Integral rocket-ramjet closed loop fuel control system

Also Published As

Publication number Publication date
FR2549146B1 (fr) 1987-12-24
US4631916A (en) 1986-12-30
GB2143282A (en) 1985-02-06
IT8421823A1 (it) 1986-01-10
JPS60173352A (ja) 1985-09-06
GB2143282B (en) 1987-07-15
IT8421823A0 (it) 1984-07-10
GB8417585D0 (en) 1984-08-15
FR2549146A1 (fr) 1985-01-18
DE3425352C2 (de) 1995-01-19
DE3425352A1 (de) 1985-01-24
JPH0370107B2 (cg-RX-API-DMAC7.html) 1991-11-06

Similar Documents

Publication Publication Date Title
IT1196185B (it) Assieme propulsivo per missile statoreattore a propulsore di accelerazione integrato
DE3273006D1 (de) Thrust reverser for a jet engine
IT8420753A0 (it) Impianto di comando per motore a turbina a gas.
IT8219723A0 (it) Gruppo di trasmissione poppiero.
IT8620138A0 (it) Ingresso per motore di aereo.
DE68900273D1 (de) Zweistoffraketenmotor.
NO893603D0 (no) Termisk isolasjon for rakettmotorhus.
DE3761916D1 (de) Raketentriebwerke.
NO153867C (no) Rakettmotor.
NO164944C (no) Kjoelesystem for en motor.
IT8483636A0 (it) Comando accessorio per motore a turbina.
DE3561344D1 (de) Thrust reverser for a jet engine
ES549623A0 (es) Un disposicion propulsora para un motor de cohete de propulsor solido.
IT8319786A0 (it) Riduttore di motore alternativo per aerei.
DE3678542D1 (de) Abwerfbares strahltriebwerk fuer flugkoerper.
IT8467545A0 (it) Assieme motore trasmissione per elicottero
GB2108641B (en) Rocket motors
IT8241667A0 (it) Apparecchiatura per il controllo di motori a propulsione.
JPS57184866A (en) Rankine engine driving refrigerator
GB2106988B (en) Rocket motors
IT1153342B (it) Gruppo di propulsione con un cambio
DE3865327D1 (de) Unterwasserauspuffgeraet fuer motorboote.
GB2305976B (en) Jet propulsion powerplants
IT8019775A0 (it) Effusore di spinta per motore di propulsione a reazione.
IT1186196B (it) Testata tattica per un razzo

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19950731