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
Application number
ES8701757A
Other languages
English (en)
Inventor
Thomas G Flock
Norman E Prevatte
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of ES2014515A6 publication Critical patent/ES2014515A6/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

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.
ES8701757A 1986-06-16 1987-06-15 Misil, conjunto de superficie aerodinamica inflable para ell metodo de mejorar su lisura aerodinamica. Expired - Fee Related ES2014515A6 (es)

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 (18)

* Cited by examiner, † Cited by third party
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
CN116202376A (zh) * 2022-12-29 2023-06-02 北京北方车辆集团有限公司 一种高阻投掷物充气膜减阻增升结构
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
WO1987007709A1 (en) 1987-12-17
CA1279790C (en) 1991-02-05
IL82760A0 (en) 1987-12-20
US4770369A (en) 1988-09-13

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19980401