IT8421823A0 - Accelerazione integrato. assieme propulsivo per missile statoreattore a propulsore di - Google Patents
Accelerazione integrato. assieme propulsivo per missile statoreattore a propulsore diInfo
- Publication number
- IT8421823A0 IT8421823A0 IT8421823A IT2182384A IT8421823A0 IT 8421823 A0 IT8421823 A0 IT 8421823A0 IT 8421823 A IT8421823 A IT 8421823A IT 2182384 A IT2182384 A IT 2182384A IT 8421823 A0 IT8421823 A0 IT 8421823A0
- Authority
- IT
- Italy
- Prior art keywords
- thrustered
- missile
- stator
- propulsion assembly
- integrated acceleration
- Prior art date
Links
- 230000001133 acceleration Effects 0.000 title 1
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)
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 true IT8421823A0 (it) | 1984-07-10 |
IT8421823A1 IT8421823A1 (it) | 1986-01-10 |
IT1196185B 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 (it) |
JP (1) | JPS60173352A (it) |
DE (1) | DE3425352C2 (it) |
FR (1) | FR2549146B1 (it) |
GB (1) | GB2143282B (it) |
IT (1) | IT1196185B (it) |
Families Citing this family (13)
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 |
US6481198B1 (en) | 1999-07-09 | 2002-11-19 | Alliant Techsystems Inc. | Multi-stage rocket motor assembly including jettisonable launch motor integrated with flight igniter |
CA2519936C (en) * | 2003-03-28 | 2008-11-18 | 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 |
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)
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 |
-
1983
- 1983-07-11 FR FR8311555A patent/FR2549146B1/fr not_active Expired
-
1984
- 1984-07-02 US US06/626,547 patent/US4631916A/en not_active Expired - Lifetime
- 1984-07-10 GB GB08417585A patent/GB2143282B/en not_active Expired
- 1984-07-10 DE DE3425352A patent/DE3425352C2/de not_active Expired - Lifetime
- 1984-07-10 IT IT21823/84A patent/IT1196185B/it active
- 1984-07-10 JP JP59141564A patent/JPS60173352A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3425352A1 (de) | 1985-01-24 |
GB2143282B (en) | 1987-07-15 |
US4631916A (en) | 1986-12-30 |
GB2143282A (en) | 1985-02-06 |
GB8417585D0 (en) | 1984-08-15 |
FR2549146B1 (fr) | 1987-12-24 |
FR2549146A1 (fr) | 1985-01-18 |
JPS60173352A (ja) | 1985-09-06 |
JPH0370107B2 (it) | 1991-11-06 |
DE3425352C2 (de) | 1995-01-19 |
IT1196185B (it) | 1988-11-10 |
IT8421823A1 (it) | 1986-01-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19950731 |