ES2161982T3 - Misil con seccion de propulsion no cilindrica. - Google Patents
Misil con seccion de propulsion no cilindrica.Info
- Publication number
- ES2161982T3 ES2161982T3 ES96305980T ES96305980T ES2161982T3 ES 2161982 T3 ES2161982 T3 ES 2161982T3 ES 96305980 T ES96305980 T ES 96305980T ES 96305980 T ES96305980 T ES 96305980T ES 2161982 T3 ES2161982 T3 ES 2161982T3
- Authority
- ES
- Spain
- Prior art keywords
- missile
- fuselage
- propulsion section
- cylindrical
- non cylindrical
- 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 - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/10—Missiles having a trajectory only in the air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
LA PRESENTE INVENCION PROPORCIONA UN MISIL (20) QUE TIENE UN FUSELAJE NO CILINDRICO (22B) POR ENCIMA DE, AL MENOS, UNA PORCION DE SU LONGITUD, CON UN SISTEMA DE PROPULSION NO CILINDRICO (34) CONTENIDO DENTRO DE LA PORCION NO CILINDRICA (22B) DEL FUSELAJE. PREFERIBLEMENTE, EL FUSELAJE (22B) Y EL SISTEMA DE PROPULSION (34) TIENEN GENERALMENTE UNA SECCION TRANSVERSAL ELIPTICA, CON UNA RAZON DE DIMENSION DEL EJE MAYOR CON RESPECTO AL EJE MENOR ENTRE MAS DE 1:1 Y 1,5:1, APROXIMADAMENTE. EL MISIL (20), ADEMAS, INCLUYE UN SISTEMA DE GUIA (38) Y UNAS CARACTERISTICAS DE CONTROL (32).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/515,479 US5677508A (en) | 1995-08-15 | 1995-08-15 | Missile having non-cylindrical propulsion section |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2161982T3 true ES2161982T3 (es) | 2001-12-16 |
Family
ID=24051528
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES96305980T Expired - Lifetime ES2161982T3 (es) | 1995-08-15 | 1996-08-15 | Misil con seccion de propulsion no cilindrica. |
Country Status (10)
Country | Link |
---|---|
US (1) | US5677508A (es) |
EP (1) | EP0768509B1 (es) |
JP (1) | JP2889193B2 (es) |
KR (1) | KR100200455B1 (es) |
AU (1) | AU687686B2 (es) |
CA (1) | CA2183279C (es) |
DE (1) | DE69616475T2 (es) |
ES (1) | ES2161982T3 (es) |
IL (1) | IL119074A (es) |
NO (1) | NO312142B1 (es) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040209344A1 (en) * | 2002-09-09 | 2004-10-21 | Pantoliano Michael W. | Crystal structure of angiotensin-converting enzyme-related carboxypeptidase |
US6871817B1 (en) | 2003-10-28 | 2005-03-29 | Raytheon Company | System containing an anamorphic optical system with window, optical corrector, and sensor |
US9151579B2 (en) * | 2009-03-24 | 2015-10-06 | Orbital Atk, Inc. | Non-circular cross-section missile components, missiles incorporating same, and methods of operation |
RU2462687C1 (ru) * | 2011-05-27 | 2012-09-27 | Николай Евгеньевич Староверов | Атмосферная жидкостная ракета (варианты) |
EP4060282B1 (en) * | 2021-03-17 | 2023-10-25 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Missile having a body forming an airfoil at an angle oblique to the longitudinal axis of the missile |
SE2100110A1 (sv) * | 2021-07-01 | 2023-01-02 | Bae Systems Bofors Ab | Projektil |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1170714B (de) * | 1959-11-26 | 1964-05-21 | Rheinmetall Gmbh | Treibladung fuer Pulverraketen |
US3121312A (en) * | 1961-02-28 | 1964-02-18 | United Aircraft Corp | Unified pitch, yaw and roll shock control |
US3202381A (en) * | 1961-11-08 | 1965-08-24 | Hans F Wuenscher | Recoverable rocket vehicle |
US3175497A (en) * | 1962-02-20 | 1965-03-30 | United Aircraft Corp | Segmented rocket engine |
GB1605395A (en) * | 1965-07-23 | 1995-04-26 | Short Brothers & Harland Ltd | Improvements in missiles |
US3491692A (en) * | 1967-02-18 | 1970-01-27 | Bolkow Gmbh | Multi-stage rocket |
US3468501A (en) * | 1967-08-29 | 1969-09-23 | Us Navy | Compatible missile/aircraft configuration |
DE1751889C3 (de) * | 1968-08-14 | 1973-11-29 | Maschinenfabrik Augsburg-Nuernberg Ag, 8000 Muenchen | Innenbrenner Feststoffrakete |
US4176813A (en) * | 1977-10-05 | 1979-12-04 | Northrop Corporation | Shark nose for aircraft |
US4369940A (en) * | 1979-12-17 | 1983-01-25 | Mcdonnell Douglas Corporation | Airbreathing propulsion system for supersonic vehicles |
US4327884A (en) * | 1980-01-23 | 1982-05-04 | The United States Of America As Represented By The Secretary Of The Air Force | Advanced air-to-surface weapon |
US5035182A (en) * | 1984-03-28 | 1991-07-30 | The United States Of America As Represented By The Secretary Of The Navy | Bending type ordnance venting device |
US4674712A (en) * | 1985-01-22 | 1987-06-23 | The Boeing Company | Double-lobe fuselage composite airplane |
DE3526472A1 (de) * | 1985-07-24 | 1987-02-05 | Messerschmitt Boelkow Blohm | Rumpfheckmodifikation von flugzeugen |
US4790350A (en) * | 1986-02-04 | 1988-12-13 | Arnold Charles M | Combat rapid assembly fuel tank |
US4736913A (en) * | 1986-09-19 | 1988-04-12 | Lockheed Corporation | Fluid flow control device |
US4815383A (en) * | 1987-08-20 | 1989-03-28 | The Boeing Company | Low cost composite missile structure |
DE3826703A1 (de) * | 1988-08-05 | 1990-02-15 | Aris Spa | Tragende flugausruestung, insbesondere fuer geschosse ballistischer art |
FR2649665B1 (fr) * | 1989-07-12 | 1991-11-08 | Airbus Ind | Fuselage de grande capacite pour avion |
FR2655722B1 (fr) * | 1989-12-12 | 1992-03-13 | Aerospatiale | Missile supersonique a pilotage en couple par spouilers. |
GB2272047B (en) * | 1989-12-14 | 1994-07-27 | British Aerospace | Stand-off weapons |
US5309712A (en) * | 1991-05-03 | 1994-05-10 | Mund Jr Charles J | Solid fuel rocket motor seals |
US5238208A (en) * | 1991-06-11 | 1993-08-24 | E-Systems, Inc. | Load mitigation system for a multi-dimensional transducer array |
-
1995
- 1995-08-15 US US08/515,479 patent/US5677508A/en not_active Expired - Lifetime
-
1996
- 1996-08-14 KR KR1019960033681A patent/KR100200455B1/ko not_active IP Right Cessation
- 1996-08-14 CA CA002183279A patent/CA2183279C/en not_active Expired - Fee Related
- 1996-08-14 IL IL11907496A patent/IL119074A/xx unknown
- 1996-08-14 NO NO19963387A patent/NO312142B1/no not_active IP Right Cessation
- 1996-08-15 DE DE69616475T patent/DE69616475T2/de not_active Expired - Lifetime
- 1996-08-15 ES ES96305980T patent/ES2161982T3/es not_active Expired - Lifetime
- 1996-08-15 JP JP8215803A patent/JP2889193B2/ja not_active Expired - Fee Related
- 1996-08-15 AU AU62091/96A patent/AU687686B2/en not_active Ceased
- 1996-08-15 EP EP96305980A patent/EP0768509B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE69616475D1 (de) | 2001-12-06 |
KR100200455B1 (ko) | 1999-06-15 |
EP0768509A3 (en) | 1998-01-07 |
US5677508A (en) | 1997-10-14 |
DE69616475T2 (de) | 2002-05-08 |
EP0768509B1 (en) | 2001-10-31 |
AU6209196A (en) | 1997-03-20 |
JPH09166399A (ja) | 1997-06-24 |
IL119074A0 (en) | 1996-11-14 |
IL119074A (en) | 1999-07-14 |
NO312142B1 (no) | 2002-03-25 |
JP2889193B2 (ja) | 1999-05-10 |
EP0768509A2 (en) | 1997-04-16 |
KR970011775A (ko) | 1997-03-27 |
NO963387L (no) | 1997-02-17 |
CA2183279A1 (en) | 1997-02-16 |
AU687686B2 (en) | 1998-02-26 |
CA2183279C (en) | 1999-12-28 |
NO963387D0 (no) | 1996-08-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA2127581A1 (fr) | Procede de preparation de spherules | |
BR9506411A (pt) | Sistema de propuls o para um veículo mais leve do que o ar | |
BR8901900A (pt) | Sistema para liberacao de uma substancia ativa para a atmosfera,matrizes e processo para formacao de um reservatorio de liberacao de substancia ativa | |
ES2192553T3 (es) | Jaula de fusion de configuracion conica. | |
BR8300458A (pt) | Recipiente com adaptacao de, pelo menos um dispositivo de memoria ativa; dispositivo de acoplamento; sistema distribuidor de fluido; complexo de aspersao de produtos quimicos agricolas; recipiente de fluido com adaptacao de, pelo menos um dispositivo de memoria ativa eletrico; e processo para realizar uma operacao que envolve ativamente o conteudo | |
ES2173469T3 (es) | Composicion de eliminacion de oxigeno de varios componentes. | |
BR9407793A (pt) | Sistema de balonete para um veículo mais leve do que o ar | |
PT99004A (pt) | Processo para a preparacao de um sistema de emulsao aquosa contendo um agente tensio-activo nao ionico | |
AR248255A1 (es) | Miembro concentrador de tensiones formador de una abertura ampliable para un envase o contenedor y un contenedor que utiliza dicho miembro. | |
BR9809497A (pt) | Sistema de suspensão de um veìculo tendo uma estrutura com dois lados opostos | |
DE69614903T2 (de) | Gerät zur Vermeidung von Flugzeugkollisionen , insbesondere mit dem Boden | |
BR9807359A (pt) | Aparelho para gerar radiação paralela para curar resina fotossensìvel | |
ES2161982T3 (es) | Misil con seccion de propulsion no cilindrica. | |
ES2058834T3 (es) | Dispositivo de separacion de dos liquidos no miscibles y utilizacion de este dispositivo para el desalado de una carga hidrocarbonada. | |
ES2148969T3 (es) | Dispositivo luminoso para la visualizacion de caracteres. | |
ES2106299T3 (es) | Procedimiento y dispositivos para cortar de forma oblicua una cinta de fibras opticas. | |
CA2297905A1 (en) | Interlingual translation system and method | |
ES2191427T3 (es) | Sistema de impacto para una columna de direccion. | |
KR870004866A (ko) | 차량용 연결포장의 이상편기 규제장치 | |
NO307143B1 (no) | Sveivstang og oeye for en sådan | |
KR900009371A (ko) | 철도차량용 구동조립체의 차축배열장치 | |
MX9300795A (es) | Funda para cassette con tarjetas separables. | |
ITTO920927A1 (it) | Veicolo con dispositivo di sicurezza per collisioni frontali. | |
ES2111469B1 (es) | Sistema de control para frenado de aeronave. | |
SE9301792D0 (sv) | Baerbalk foer en bestrykningsanordning |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 768509 Country of ref document: ES |