DE602007008387D1 - Nasenkegel für eine verbundrakete - Google Patents

Nasenkegel für eine verbundrakete

Info

Publication number
DE602007008387D1
DE602007008387D1 DE602007008387T DE602007008387T DE602007008387D1 DE 602007008387 D1 DE602007008387 D1 DE 602007008387D1 DE 602007008387 T DE602007008387 T DE 602007008387T DE 602007008387 T DE602007008387 T DE 602007008387T DE 602007008387 D1 DE602007008387 D1 DE 602007008387D1
Authority
DE
Germany
Prior art keywords
connector
nose cone
nose
cone
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.)
Active
Application number
DE602007008387T
Other languages
English (en)
Inventor
Andrew B Facciano
Robert T Moore
Gregg J Hlavacek
Craig D Seasly
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
Raytheon 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 Raytheon Co filed Critical Raytheon Co
Publication of DE602007008387D1 publication Critical patent/DE602007008387D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2246—Active homing systems, i.e. comprising both a transmitter and a receiver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2286—Homing guidance systems characterised by the type of waves using radio waves
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/281—Nose antennas
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061—Two dimensional planar arrays
    • H01Q21/065—Patch antenna array

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Astronomy & Astrophysics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Details Of Aerials (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
DE602007008387T 2006-03-31 2007-01-26 Nasenkegel für eine verbundrakete Active DE602007008387D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/395,794 US7681834B2 (en) 2006-03-31 2006-03-31 Composite missile nose cone
PCT/US2007/002101 WO2008045125A2 (en) 2006-03-31 2007-01-26 Composite missile nose cone

Publications (1)

Publication Number Publication Date
DE602007008387D1 true DE602007008387D1 (de) 2010-09-23

Family

ID=38557389

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007008387T Active DE602007008387D1 (de) 2006-03-31 2007-01-26 Nasenkegel für eine verbundrakete

Country Status (8)

Country Link
US (1) US7681834B2 (de)
EP (1) EP2002197B1 (de)
JP (1) JP2009532251A (de)
AU (1) AU2007307309B2 (de)
CA (1) CA2641078C (de)
DE (1) DE602007008387D1 (de)
IL (1) IL193057A (de)
WO (1) WO2008045125A2 (de)

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US8074516B2 (en) * 2008-06-26 2011-12-13 Raytheon Company Methods and apparatus for non-axisymmetric radome
JP5320278B2 (ja) * 2009-12-22 2013-10-23 川崎重工業株式会社 飛行体用レドーム
US8789390B2 (en) 2010-04-15 2014-07-29 Corning Incorporated Near net fused silica articles and method of making
US20130280470A1 (en) 2012-04-20 2013-10-24 Julian Norly Thermal Management For Aircraft Composites
CN104685710B (zh) 2012-08-17 2016-11-23 莱尔德技术股份有限公司 多频带天线组件
US9112275B2 (en) 2012-09-05 2015-08-18 Raytheon Company Radome film
JP5510980B1 (ja) * 2013-02-15 2014-06-04 防衛省技術研究本部長 飛翔体
US10333210B2 (en) 2013-03-15 2019-06-25 Intel Corporation Low profile high performance integrated antenna for small cell base station
DE102013102812B4 (de) * 2013-03-19 2017-01-26 Airbus Operations Gmbh Rumpfstruktur für ein Verkehrsmittel, Verkehrsmittel und Verfahren zum Herstellen einer Rumpfstruktur für ein Verkehrsmittel
CN104425879B (zh) * 2013-09-03 2017-12-29 深圳光启创新技术有限公司 共形天线、制造共形天线的方法及材料
US9676469B2 (en) * 2014-04-10 2017-06-13 Lockheed Martin Corporation System and method for fastening structures
RU2566643C1 (ru) * 2014-07-08 2015-10-27 Акционерное общество "Обнинское научно-производственное предприятие "Технология"им. А.Г.Ромашина Способ соединения керамического обтекателя с металлическим корпусом летательного аппарата
US9711845B2 (en) * 2014-07-21 2017-07-18 The Boeing Company Aerial vehicle radome assembly and methods for assembling the same
US9933097B2 (en) 2014-07-30 2018-04-03 Simmonds Precision Products, Inc. Ring couplings
CN104511861B (zh) * 2014-11-12 2016-09-07 上海无线电设备研究所 一种天线罩用六导柱可移动定位装置
US9835425B2 (en) 2015-08-14 2017-12-05 Raytheon Company Metallic nosecone with unitary assembly
US9647330B1 (en) * 2015-10-21 2017-05-09 The Boeing Company Whisker reinforced high fracture toughness ceramic tips for radomes
RU2650725C1 (ru) * 2016-07-08 2018-04-17 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Антенный обтекатель и способ его изготовления
FR3055050B1 (fr) * 2016-08-11 2019-11-22 Thales Radar a commande en site-roulis pour le guidage autonome d'une plateforme et missile autoguide comprenant un tel radar
DE102018005406B3 (de) 2018-07-06 2019-09-05 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Penetrator
FR3099132B1 (fr) * 2019-07-26 2022-01-28 Mbda France Capot pour vehicule, en particulier pour vehicule supersonique ou hypersonique
EP4032144A4 (de) * 2019-09-20 2022-11-16 Aselsan Elektronik Sanayi ve Ticaret Anonim Sirketi Verfahren zur herstellung keramischer mehrschichtstrukturen durch endlosfäden mit gleicher zusammensetzung
US11964917B2 (en) 2019-09-20 2024-04-23 Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi Fabrication method of functionally-graded structures by continuous ceramic filaments
US11901619B2 (en) * 2021-12-16 2024-02-13 The Boeing Company Radome with ceramic matrix composite
CN114286559B (zh) * 2021-12-23 2023-07-11 航天科工微电子系统研究院有限公司 一种导引头头罩安装结构

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US3063654A (en) * 1959-02-03 1962-11-13 Fred R Youngren Radome with boresight error reduction means
US3314070A (en) * 1959-04-30 1967-04-11 Fred R Youngren Tapered radomes
US3858214A (en) * 1966-05-18 1974-12-31 Us Army Antenna system
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US3820118A (en) * 1972-12-08 1974-06-25 Bendix Corp Antenna and interface structure for use with radomes
US4121002A (en) * 1977-07-06 1978-10-17 The United States Of America As Represented By The Secretary Of The Air Force Fabrication of antenna windows
US4240596A (en) * 1978-07-28 1980-12-23 General Dynamics Corporation, Pomona Division Articulated eyeball radome
US4210804A (en) * 1978-08-22 1980-07-01 Raytheon Company Free-gyro optical seeker
US4451833A (en) * 1980-05-15 1984-05-29 Rogers Corporation Radome formed of segmented rings of fiber-PTFE composite
US4415130A (en) * 1981-01-12 1983-11-15 Westinghouse Electric Corp. Missile system with acceleration induced operational energy
US4431996A (en) * 1981-12-03 1984-02-14 The United States Of America As Represented By The Secretary Of The Air Force Missile multi-frequency antenna
DE3243823A1 (de) * 1982-11-26 1984-05-30 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Schnappverbindung zwischen koerpern
US4520973A (en) * 1983-04-11 1985-06-04 The United States Of America As Represented By The Secretary Of The Navy Stabilized gimbal platform
US4600166A (en) * 1984-06-11 1986-07-15 Allied Corporation Missile having reduced mass guidance system
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US5129990A (en) * 1988-12-19 1992-07-14 Hughes Aircraft Company Method for producing a gas-tight radome-to-fuselage structural bond
FR2656081B1 (fr) * 1989-12-19 1992-02-28 Thomson Brandt Armements Enveloppe peripherique pour une munition guidee tiree par effet canon.
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US6037023A (en) * 1994-07-08 2000-03-14 Raytheon Company Broadband composite structure fabricated from inorganic polymer matrix reinforced with glass or ceramic woven cloth
US5483894A (en) * 1994-12-27 1996-01-16 Hughes Missile Systems Company Integral missile antenna-fuselage assembly
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US5707723A (en) * 1996-02-16 1998-01-13 Mcdonnell Douglas Technologies, Inc. Multilayer radome structure and its fabrication
JPH1013129A (ja) * 1996-06-25 1998-01-16 Sumitomo Electric Ind Ltd レドーム
DE19632893C2 (de) * 1996-08-16 2001-02-08 Industrieanlagen Betr Sgmbh Ia Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik
US5982339A (en) * 1996-11-26 1999-11-09 Ball Aerospace & Technologies Corp. Antenna system utilizing a frequency selective surface
DE19735452C2 (de) * 1997-08-16 1999-07-22 Bodenseewerk Geraetetech Rohrverbindung, insbesondere zum Verbinden zweier rohrförmiger Rumpfteile eines Flugkörpers
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US6407711B1 (en) * 2001-04-24 2002-06-18 Science And Applied Technology, Inc. Antenna array apparatus with conformal mounting structure
US6526860B2 (en) 2001-06-19 2003-03-04 Raytheon Company Composite concentric launch canister
CA2401915C (en) * 2001-09-11 2007-01-09 Matsushita Electric Industrial Co., Ltd. Polymer elecrolyte fuel cell
US6531989B1 (en) 2001-11-14 2003-03-11 Raytheon Company Far field emulator for antenna calibration
US20040056818A1 (en) * 2002-09-25 2004-03-25 Victor Aleksandrovich Sledkov Dual polarised antenna
US6731245B1 (en) 2002-10-11 2004-05-04 Raytheon Company Compact conformal patch antenna
DE102004044203B4 (de) 2004-09-13 2006-12-07 Diehl Bgt Defence Gmbh & Co. Kg Materialverbundfenster

Also Published As

Publication number Publication date
WO2008045125A3 (en) 2008-06-12
EP2002197B1 (de) 2010-08-11
US7681834B2 (en) 2010-03-23
AU2007307309A1 (en) 2008-04-17
JP2009532251A (ja) 2009-09-10
EP2002197A2 (de) 2008-12-17
WO2008045125A2 (en) 2008-04-17
CA2641078C (en) 2010-12-07
IL193057A0 (en) 2009-02-11
CA2641078A1 (en) 2008-04-17
AU2007307309B2 (en) 2010-06-03
IL193057A (en) 2012-08-30
US20070228211A1 (en) 2007-10-04

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