ES2014515A6 - Misil, conjunto de superficie aerodinamica inflable para ell metodo de mejorar su lisura aerodinamica. - Google Patents
Misil, conjunto de superficie aerodinamica inflable para ell metodo de mejorar su lisura aerodinamica.Info
- Publication number
- ES2014515A6 ES2014515A6 ES8701757A ES8701757A ES2014515A6 ES 2014515 A6 ES2014515 A6 ES 2014515A6 ES 8701757 A ES8701757 A ES 8701757A ES 8701757 A ES8701757 A ES 8701757A ES 2014515 A6 ES2014515 A6 ES 2014515A6
- Authority
- ES
- Spain
- Prior art keywords
- inflatable
- forward end
- membrane
- missile
- aerodynamic
- 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 - Fee Related
Links
- 239000012528 membrane Substances 0.000 abstract 3
- 239000000523 sample Substances 0.000 abstract 2
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
Abstract
MISIL, CONJUNTO DE SUPERFICIE AERODINAMICA INFLABLE PARA EL Y METODO DE MEJORAR SU LISURA AERODINAMICA. SE CONSTRIYE UNA SUPERFICIE AERODINAMICA INFLABLE (14) ADAPTADA PARTICULARMENTE PARA MEJORAR LA LISURA AERODINAMICA DEL EXTREMO DELANTERO DE UN MISIL DEL TIPO QUE TIENE UN EXTREMO DELANTERO RELATIVAMENTE ROMO CON UNA PIEZA SONDA EXTENSIBLE (26) DISPUESTA CENTRALMENTE. SE DISPONE UNA MEMBRANA FLEXIBLE (36) QUE TIENE UN BORDE DE BASE (46) FIJADO HERMETICAMENTE AL BORDE DELANTERO DE LA CUBIERTA DEL MISIL Y UN VERTICE (48) FIJADO AL EXTREMO DELANTERO DE LA SONDA (26). LA MEMBRANA (36) ES INFLADA POR UN GENERADOR DE GAS (42) PARA PRESURIZAR EL INTERIOR DE LA MEMBRANA PARA DEFINIR UNA SUPERFICIE FRONTAL LISA AERODINAMICA EN FORMA DE OJIVA. EL INVENTO ES UTIL PARA PROPORCIONAR CARACTERISTICAS DE VUELO MEJORADAS A LOS MISILES BALISTICOS.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/874,985 US4770369A (en) | 1986-06-16 | 1986-06-16 | Inflatable missle airframe surfaces |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2014515A6 true ES2014515A6 (es) | 1990-07-16 |
Family
ID=25365014
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES8701757A Expired - Fee Related ES2014515A6 (es) | 1986-06-16 | 1987-06-15 | Misil, conjunto de superficie aerodinamica inflable para ell metodo de mejorar su lisura aerodinamica. |
Country Status (5)
Country | Link |
---|---|
US (1) | US4770369A (es) |
CA (1) | CA1279790C (es) |
ES (1) | ES2014515A6 (es) |
IL (1) | IL82760A0 (es) |
WO (1) | WO1987007709A1 (es) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2171415T3 (es) * | 1992-06-29 | 2002-09-16 | United Solar Systems Corp | Proceso de deposicion activada por microondas con regulacion de la temperatura del sustrato. |
IL107830A (en) * | 1993-12-01 | 1998-07-15 | Israel State | Controlled scanner head missile |
US5464172A (en) * | 1994-05-26 | 1995-11-07 | Lockheed Missiles & Space Company, Inc. | Deployable mass and sensor for improved missile control |
US5460676A (en) * | 1994-05-27 | 1995-10-24 | Lockheed Missiles & Space Company, Inc. | Fabrication method for inflatable nose fairing |
US5463957A (en) * | 1994-05-26 | 1995-11-07 | Lockheed Missiles & Space Company, Inc. | Inflatable nose fairing |
US5494239A (en) * | 1994-08-02 | 1996-02-27 | Loral Vought Systems Corporation | Expandable ogive |
US5725709A (en) * | 1995-10-13 | 1998-03-10 | Lockheed Missiles & Space Co., Inc. | Fabrication method for an inflatable deployable control structure for aerospace vehicles |
SE513893C2 (sv) * | 1999-04-14 | 2000-11-20 | Bofors Weapon Sys Ab | Sätt och anordning för bromsning av i ballistiska banor flygande projektiler |
US6388184B1 (en) * | 2000-10-04 | 2002-05-14 | The United States Of America As Represented By The Secretary Of The Navy | Deployable nose for an underwater vehicle |
US6862996B2 (en) * | 2002-10-15 | 2005-03-08 | Mark Key | Projectile for rapid fire gun |
JP3916084B2 (ja) * | 2004-04-30 | 2007-05-16 | 独立行政法人 宇宙航空研究開発機構 | 伸展式ノーズコーンを用いた飛翔体の抵抗低減方法 |
US7874251B1 (en) * | 2007-04-12 | 2011-01-25 | Lockheed Martin Corporation | Cavity-running projectile having a telescoping nose |
US8146501B1 (en) * | 2008-03-03 | 2012-04-03 | Lockheed Martin Corporation | Supercavitating projectile having a morphable nose |
US9132908B1 (en) * | 2013-03-15 | 2015-09-15 | The Boeing Company | Expandable nose cone |
IL238372B (en) | 2015-04-19 | 2020-03-31 | Israel Aerospace Ind Ltd | A missile and a warhead system for it |
US10928169B2 (en) * | 2019-02-07 | 2021-02-23 | Bae Systems Rokar International Ltd. | Seal for a projectile guiding kit |
CN116067240B (zh) * | 2023-02-20 | 2024-04-05 | 北京理工大学 | 一种导弹高速入水充气降载装置 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2377839A (en) * | 1943-04-05 | 1945-06-05 | Lewis B Lee | Projectile for guns |
US3086467A (en) * | 1959-05-15 | 1963-04-23 | John J Gallagher | Gas operated extendible probe for ballistic model |
US3053488A (en) * | 1959-05-29 | 1962-09-11 | Martin Marietta Corp | Inflatable streamlined enclosure |
US3710716A (en) * | 1970-07-28 | 1973-01-16 | Boeing Co | Ram pressure standoff extension and safe/arm mechanism for self-arming munitions |
US4166597A (en) * | 1974-05-09 | 1979-09-04 | The United States Of America As Represented By The Secretary Of The Air Force | Stowable and inflatable vehicle |
DE2645419A1 (de) * | 1976-10-08 | 1978-04-13 | Messerschmitt Boelkow Blohm | Hohlladungsmunition |
DE3237485A1 (de) * | 1982-10-09 | 1984-04-12 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Entfaltbares sensorsystem |
DE3332241A1 (de) * | 1983-09-07 | 1985-03-21 | Dynamit Nobel Ag, 5210 Troisdorf | Hohlladung |
DE3343267A1 (de) * | 1983-11-30 | 1985-06-05 | Rheinmetall GmbH, 4000 Düsseldorf | Luftverlastbare einrichtung zur erzeugung eines projektils |
DE3347005A1 (de) * | 1983-12-24 | 1985-07-04 | Dynamit Nobel Ag, 5210 Troisdorf | Flugkoerper |
US4549464A (en) * | 1984-02-23 | 1985-10-29 | Morton Thiokol, Inc. | Inflatable, aerodynamic shroud |
-
1986
- 1986-06-16 US US06/874,985 patent/US4770369A/en not_active Expired - Lifetime
-
1987
- 1987-06-02 IL IL82760A patent/IL82760A0/xx not_active IP Right Cessation
- 1987-06-05 WO PCT/US1987/001315 patent/WO1987007709A1/en unknown
- 1987-06-15 ES ES8701757A patent/ES2014515A6/es not_active Expired - Fee Related
- 1987-06-15 CA CA000539612A patent/CA1279790C/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
WO1987007709A1 (en) | 1987-12-17 |
US4770369A (en) | 1988-09-13 |
CA1279790C (en) | 1991-02-05 |
IL82760A0 (en) | 1987-12-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES2014515A6 (es) | Misil, conjunto de superficie aerodinamica inflable para ell metodo de mejorar su lisura aerodinamica. | |
GB8627581D0 (en) | Gas turbine jet propulsion unit | |
DE3888773D1 (de) | Druckgefäss. | |
BR8706890A (pt) | Dispositivo de escapamento de uma turbina a gas,constituido de um difusor de jatos | |
ES475238A1 (es) | Perfeccionamientos en planchas de vela con aleta adicional. | |
EP0223321A3 (en) | Life saving device | |
DE3877096D1 (de) | Querstrahlruder, insbesondere bugstrahlruder, fuer schiffe. | |
GB1460947A (en) | Displacement ducted craft | |
FR2410599A2 (fr) | Perfectionnements aux engins a voile | |
DE3764344D1 (de) | Bewegliches gelenk fuer verbindungsstuecke. | |
ATE211095T1 (de) | Flugzeug und verfahren zum gebrauch | |
GB2216959B (en) | Air turbine or propellor | |
GB1492030A (en) | Mast | |
GB2003807A (en) | Aircraft | |
ES255441U (es) | Bote neumatico | |
ES2009796B3 (es) | Perfeccionamientos introducidos en los ingenios de navegacion a vela. | |
GB2022707B (en) | Jet pumps particulariy for ballasting and de-ballasting ships | |
JPS5387495A (en) | Catamaran equipped with common side thruster | |
JPS5247295A (en) | Apparatus for keeping a ship at a standstill | |
KR900004593A (ko) | 인력 구동 썰핑 보우트의 추진체 | |
FR2783497B1 (fr) | Avion a aile supercritique a faible trainee d'onde | |
SE8603932L (sv) | Kalkningsbat | |
KR880007321A (ko) | 오뚜기 호흡 수중 마스크 | |
ES8505600A1 (es) | Nuevo sistema de flotacion para vehiculos acuaticos | |
KR890014885A (ko) | 부력과 중력의 동력 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 19980401 |