IT8967342A0 - Propulsore missilistico senza ugel lo a piccolo allungamento - Google Patents
Propulsore missilistico senza ugel lo a piccolo allungamentoInfo
- Publication number
 - IT8967342A0 IT8967342A0 IT8967342A IT6734289A IT8967342A0 IT 8967342 A0 IT8967342 A0 IT 8967342A0 IT 8967342 A IT8967342 A IT 8967342A IT 6734289 A IT6734289 A IT 6734289A IT 8967342 A0 IT8967342 A0 IT 8967342A0
 - Authority
 - IT
 - Italy
 - Prior art keywords
 - extendance
 - thruster
 - missile
 - nozzle
 - small
 - Prior art date
 
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
 - 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
 - F02K7/105—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 using a solid fuel
 
 - 
        
- 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
 - F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
 - F02K9/10—Shape or structure of solid propellant charges
 
 - 
        
- 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
 - F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
 - F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle
 
 
Landscapes
- Engineering & Computer Science (AREA)
 - Chemical & Material Sciences (AREA)
 - Combustion & Propulsion (AREA)
 - Mechanical Engineering (AREA)
 - General Engineering & Computer Science (AREA)
 - Exhaust Gas After Treatment (AREA)
 - Air Bags (AREA)
 - Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
 - Portable Nailing Machines And Staplers (AREA)
 - Testing Of Engines (AREA)
 - Fuel-Injection Apparatus (AREA)
 - Plasma Technology (AREA)
 - Nozzles (AREA)
 
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title | 
|---|---|---|---|
| FR8806263A FR2631387B1 (fr) | 1988-05-10 | 1988-05-10 | Propulseur sans tuyere de faible allongement | 
Publications (2)
| Publication Number | Publication Date | 
|---|---|
| IT8967342A0 true IT8967342A0 (it) | 1989-05-09 | 
| IT1232272B IT1232272B (it) | 1992-01-28 | 
Family
ID=9366154
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date | 
|---|---|---|---|
| IT8967342A IT1232272B (it) | 1988-05-10 | 1989-05-09 | Propulsore missilistico senza ugello a piccolo allungamento | 
Country Status (10)
| Country | Link | 
|---|---|
| US (1) | US5125229A (it) | 
| JP (1) | JPH0278758A (it) | 
| AU (1) | AU632478B2 (it) | 
| CH (1) | CH678648A5 (it) | 
| DE (1) | DE3915148C2 (it) | 
| ES (1) | ES2013469A6 (it) | 
| FR (1) | FR2631387B1 (it) | 
| GB (1) | GB2218494B (it) | 
| IT (1) | IT1232272B (it) | 
| SE (1) | SE465935B (it) | 
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| FR2863665B1 (fr) * | 1988-10-12 | 2007-03-30 | Aerospatiale | Statoreacteur a structure tubulaire et missile propulse par un tel statoreacteur | 
| SE468647B (sv) * | 1991-06-14 | 1993-02-22 | Foersvarets Forskningsanstalt | Rammotor med fast braensle foer t ex en rotationsstabiliserad projektil | 
| US5787703A (en) * | 1996-05-10 | 1998-08-04 | Fougerousse; Russell | Combined ramjet and rocket engine having rectilinear duct | 
| DE19635847C2 (de) * | 1996-09-04 | 1998-07-16 | Daimler Benz Aerospace Ag | Lenkflugkörper mit Staustrahlantrieb | 
| FR2764645B1 (fr) * | 1997-06-16 | 1999-08-20 | Aerospatiale | Chargement de propergol solide pour propulseur et propulseur muni d'un tel chargement | 
| RU2125175C1 (ru) * | 1998-02-20 | 1999-01-20 | Пермский завод им.С.М.Кирова | Ракетный двигатель твердого топлива | 
| RU2175399C2 (ru) * | 1999-07-29 | 2001-10-27 | Южно-Российский государственный технический университет | Способ регулирования скорости горения высокоэнергетичной конденсированной системы | 
| US7306715B2 (en) | 2002-08-05 | 2007-12-11 | Denso Corporation | Pump module | 
| RU2289036C2 (ru) * | 2005-02-22 | 2006-12-10 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" | Твердотопливный газогенератор для катапультного устройства ракеты | 
| FR3089568B1 (fr) * | 2018-12-05 | 2021-05-28 | Centre Nat Etd Spatiales | Propulseur solide pour lanceur | 
| CN112177797B (zh) * | 2020-09-16 | 2021-11-05 | 西北工业大学 | 一种无喷管固体火箭发动机 | 
| CN113006967B (zh) * | 2021-02-08 | 2022-04-19 | 中国人民解放军国防科技大学 | 一种火箭与前缘突扩凹腔组合的rbcc内流道 | 
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| FR1003758A (fr) * | 1947-02-21 | 1952-03-21 | Soc Tech De Rech Ind | Perfectionnements aux réacteurs utilisés pour la propulsion par réaction | 
| FR1095546A (fr) * | 1953-12-10 | 1955-06-03 | Soc Tech De Rech Ind | Propulseur | 
| US2906094A (en) * | 1954-04-14 | 1959-09-29 | Glenn H Damon | Fuel and rapid ignition apparatus for ignition of fuel in ram jets and rockets | 
| FR1265327A (fr) * | 1960-05-19 | 1961-06-30 | France Etat | Dispositif d'allumage du propulseur de croisière d'un projectile autopropulsé | 
| US3319424A (en) * | 1965-09-30 | 1967-05-16 | Frederick L Haake | Method and means for supporting a ram-jet propellant | 
| DE1626069B1 (de) * | 1967-10-18 | 1970-10-08 | Messerschmitt Boelkow Blohm | Kombinationstriebwerk | 
| US3557556A (en) * | 1968-05-20 | 1971-01-26 | Us Air Force | Thrust modulator for hybrid rockets | 
| DE2230457C3 (de) * | 1972-06-22 | 1981-05-27 | Dynamit Nobel Ag, 5210 Troisdorf | Zwischenwand für Raketentriebwerke | 
| US4277940A (en) * | 1979-07-25 | 1981-07-14 | United Technologies Corporation | Integral rocket-ramjet closed loop fuel control system | 
| JPS57131845A (en) * | 1981-02-06 | 1982-08-14 | Nissan Motor Co Ltd | Ram rocket | 
| US4332631A (en) * | 1982-03-04 | 1982-06-01 | Hercules Incorporated | Castable silicone based magnesium fueled propellant | 
| GB8324900D0 (en) * | 1983-09-16 | 1983-10-19 | Secr Defence | Rocket motors | 
| JPS60142043A (ja) * | 1983-12-28 | 1985-07-27 | Tech Res & Dev Inst Of Japan Def Agency | ラムロケツトの保炎装置 | 
| DE3407901A1 (de) * | 1984-03-03 | 1985-09-05 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Kombinierte schubduese fuer rueckstosstriebwerke, insbesondere raketen-staubstrahltriebwerke | 
| US4578947A (en) * | 1984-12-24 | 1986-04-01 | The United States Of America As Represented By The Secretary Of The Army | Single cast rod-in-tube solid propellant rocket motor grain with a torispherical dome | 
- 
        1988
        
- 1988-05-10 FR FR8806263A patent/FR2631387B1/fr not_active Expired - Lifetime
 
 - 
        1989
        
- 1989-04-18 CH CH1479/89A patent/CH678648A5/fr not_active IP Right Cessation
 - 1989-04-26 GB GB8909465A patent/GB2218494B/en not_active Expired - Lifetime
 - 1989-04-28 AU AU33770/89A patent/AU632478B2/en not_active Ceased
 - 1989-04-28 ES ES898901486A patent/ES2013469A6/es not_active Expired - Lifetime
 - 1989-05-03 SE SE8901594A patent/SE465935B/sv not_active IP Right Cessation
 - 1989-05-09 IT IT8967342A patent/IT1232272B/it active
 - 1989-05-09 DE DE3915148A patent/DE3915148C2/de not_active Expired - Fee Related
 - 1989-05-09 JP JP1114319A patent/JPH0278758A/ja active Pending
 
 - 
        1990
        
- 1990-10-23 US US07/603,878 patent/US5125229A/en not_active Expired - Fee Related
 
 
Also Published As
| Publication number | Publication date | 
|---|---|
| GB8909465D0 (en) | 1989-06-14 | 
| DE3915148A1 (de) | 1989-11-23 | 
| ES2013469A6 (es) | 1990-05-01 | 
| CH678648A5 (it) | 1991-10-15 | 
| FR2631387B1 (fr) | 1990-07-13 | 
| GB2218494B (en) | 1992-01-15 | 
| JPH0278758A (ja) | 1990-03-19 | 
| DE3915148C2 (de) | 1998-07-23 | 
| US5125229A (en) | 1992-06-30 | 
| AU3377089A (en) | 1989-11-16 | 
| FR2631387A1 (fr) | 1989-11-17 | 
| SE8901594D0 (sv) | 1989-05-03 | 
| SE465935B (sv) | 1991-11-18 | 
| GB2218494A (en) | 1989-11-15 | 
| SE8901594L (sv) | 1989-11-11 | 
| IT1232272B (it) | 1992-01-28 | 
| AU632478B2 (en) | 1993-01-07 | 
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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: 19970530  |