WO2005103600A3 - Missile with multiple nosecones - Google Patents

Missile with multiple nosecones Download PDF

Info

Publication number
WO2005103600A3
WO2005103600A3 PCT/US2004/034567 US2004034567W WO2005103600A3 WO 2005103600 A3 WO2005103600 A3 WO 2005103600A3 US 2004034567 W US2004034567 W US 2004034567W WO 2005103600 A3 WO2005103600 A3 WO 2005103600A3
Authority
WO
WIPO (PCT)
Prior art keywords
assembly
different
payload assembly
nosecones
nosecone
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.)
Ceased
Application number
PCT/US2004/034567
Other languages
French (fr)
Other versions
WO2005103600A2 (en
Inventor
Andrew B Facciano
Robert T Moore
James E Parry
John T White
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
Priority to JP2006539521A priority Critical patent/JP4444964B2/en
Priority to EP04821768A priority patent/EP1685362B1/en
Priority to DE602004008664T priority patent/DE602004008664T2/en
Publication of WO2005103600A2 publication Critical patent/WO2005103600A2/en
Publication of WO2005103600A3 publication Critical patent/WO2005103600A3/en
Priority to IL173568A priority patent/IL173568A/en
Anticipated expiration legal-status Critical
Ceased 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
    • 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
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Pens And Brushes (AREA)
  • Semiconductor Lasers (AREA)
  • Advance Control (AREA)

Abstract

A missile (10) includes a payload assembly (16) that has a pair of nosecones (18, 20). The nosecones may be optimized for different environments and/or phases of flight, for example, having different shapes, different shell materials, different types of seals, and/or different separation mechanisms. The first (outer) nosecone (18) may have a more streamlined shape, be made of more thermally-protective material, and may meet less stringent sealing requirements, than the second (inner) nosecone (20). Separation of the outer nosecone from the payload assembly may cause backward movement of a center of pressure of the payload assembly, bringing the center of pressure of the assembly closer to a center of gravity of the assembly. This may make the payload assembly easier to maneuver, for example, reducing or eliminating the need for intervention by an attitude control system, to maintain the payload assembly on a desired course.
PCT/US2004/034567 2003-11-17 2004-10-19 Missile with multiple nosecones Ceased WO2005103600A2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2006539521A JP4444964B2 (en) 2003-11-17 2004-10-19 Missile with multiple nose cones
EP04821768A EP1685362B1 (en) 2003-11-17 2004-10-19 Missile with multiple nosecones
DE602004008664T DE602004008664T2 (en) 2003-11-17 2004-10-19 STOREY WITH MULTIPLE NOSE CONE
IL173568A IL173568A (en) 2003-11-17 2006-02-06 Missile with multiple axially distanced nosecones

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/715,176 2003-11-17
US10/715,176 US7082878B2 (en) 2003-07-01 2003-11-17 Missile with multiple nosecones

Publications (2)

Publication Number Publication Date
WO2005103600A2 WO2005103600A2 (en) 2005-11-03
WO2005103600A3 true WO2005103600A3 (en) 2005-12-08

Family

ID=35034365

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2004/034567 Ceased WO2005103600A2 (en) 2003-11-17 2004-10-19 Missile with multiple nosecones

Country Status (7)

Country Link
US (1) US7082878B2 (en)
EP (1) EP1685362B1 (en)
JP (1) JP4444964B2 (en)
AT (1) ATE371848T1 (en)
DE (1) DE602004008664T2 (en)
IL (1) IL173568A (en)
WO (1) WO2005103600A2 (en)

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AU2005210590B2 (en) * 2004-02-10 2008-03-13 Federal State Unitary Enterprise "State Research And Production Enterprise "Bazalt" Method and device for controlling and/or putting out fires
DE102005030090B4 (en) * 2005-06-27 2007-03-22 Diehl Bgt Defence Gmbh & Co. Kg Throw-off hood and missile with detachable hood
US20070260894A1 (en) * 2006-05-03 2007-11-08 Aguilar Maximino Jr Optimizing thermal performance using feed-back directed optimization
US8156867B2 (en) * 2006-07-17 2012-04-17 Raytheon Company Methods and apparatus for multiple part missile
IL189089A0 (en) * 2008-01-28 2008-08-07 Rafael Advanced Defense Sys Apparatus and method for splitting and removing a shroud from an airborne vehicle
WO2009105312A2 (en) * 2008-01-31 2009-08-27 The Penn State Research Foundation Removable protective nose cover
IL201585A (en) * 2009-10-15 2014-05-28 Rafael Advanced Defense Sys Missile nose fairing system
US8485475B2 (en) * 2009-12-16 2013-07-16 Daniel W. Allen Debris removal management system and method of operation thereof
DE102010007064B4 (en) * 2010-02-06 2012-03-29 Diehl Bgt Defence Gmbh & Co. Kg Missile head and method of separating a hood from a missile body
US8350201B2 (en) 2010-10-14 2013-01-08 Raytheon Company Systems, apparatus and methods to compensate for roll orientation variations in missile components
US8878110B2 (en) * 2010-12-14 2014-11-04 Raytheon Company Projectile that includes propulsion system and launch motor on opposing sides of payload and method
RU2486461C2 (en) * 2011-09-20 2013-06-27 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Cruise missile
KR101265090B1 (en) * 2011-10-20 2013-05-16 국방과학연구소 Separation apparatus for cap of flight vehicle and flight vehicle having the same
US8931738B2 (en) * 2012-02-21 2015-01-13 Raytheon Company Releasable radome cover
RU2492413C1 (en) * 2012-03-05 2013-09-10 Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" Drop head fairing of aircraft (versions)
US8955791B2 (en) * 2012-05-10 2015-02-17 The Boeing Company First and second stage aircraft coupled in tandem
RU2502042C1 (en) * 2012-05-22 2013-12-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Тульский государственный университет" (ТулГУ) Guided jet projectile
US9018572B2 (en) 2012-11-06 2015-04-28 Raytheon Company Rocket propelled payload with divert control system within nose cone
KR101473729B1 (en) 2013-05-15 2014-12-18 국방과학연구소 Apparatus for opening the nose cap of flying object
US10189578B2 (en) * 2013-06-12 2019-01-29 The Boeing Company Self-balancing pressure bulkhead
US11548664B1 (en) * 2013-06-24 2023-01-10 Charl E. Janeke System, apparatus, and methods for a nosecone and propulsive nozzle
US10279932B2 (en) * 2016-03-28 2019-05-07 Charl Emelio Janeke System, apparatus and methods for a nosecone and a propulsive nozzle of an airspace plane
US9121668B1 (en) 2014-02-13 2015-09-01 Raytheon Company Aerial vehicle with combustible time-delay fuse
IL232381B (en) 2014-04-30 2020-02-27 Israel Aerospace Ind Ltd Cover
FR3022995B1 (en) * 2014-06-25 2017-06-09 Mbda France MISSILE PROVIDED WITH A SEPARABLE PROTECTIVE VEST
FR3022885B1 (en) * 2014-06-25 2016-10-21 Mbda France STRUCTURING WALL OF MISSILE, ESPECIALLY FOR THERMAL PROTECTION COFFEE
DE102014011035A1 (en) * 2014-07-23 2016-01-28 Diehl Bgt Defence Gmbh & Co. Kg Hull hood for a missile
US9857154B2 (en) * 2014-07-30 2018-01-02 The United States Of America As Represented By The Secretary Of The Army Steerable munitions projectile
US20170144761A1 (en) * 2015-11-19 2017-05-25 A.L.D. Advanced Logistics Development Ltd. Detachable Pilotable Capsules and Aircrafts Including Detachable Pilotable Capsules
US10353064B2 (en) * 2016-05-26 2019-07-16 Decisive Analytics Corporation Method and apparatus for detecting airborne objects
IL248966B2 (en) 2016-11-14 2023-02-01 Elta Systems Ltd Methods and systems for detecting and/or tracking projectile
US10030952B1 (en) 2017-03-30 2018-07-24 The United States Of America As Represented By The Secretary Of The Army Thermally deployable shroud for affordable precision guided projectile
FR3065521B1 (en) 2017-04-21 2019-06-28 Mbda France MISSILE PROVIDED WITH A SEPARABLE HEADBOARD COMPRISING AT LEAST ONE EJECTABLE SHELL COOPERATING WITH A SUPPORTING ELEMENT
FR3065798A1 (en) * 2017-04-28 2018-11-02 Mbda France ACTUATING DEVICE FOR EJECTING AT LEAST ONE REMOVABLE PORTION OF MISSILE, ESPECIALLY A HEAD
US11852447B2 (en) * 2019-04-26 2023-12-26 The University Of Kansas Maneuvering aeromechanically stable sabot system
WO2020218569A1 (en) * 2019-04-26 2020-10-29 川崎重工業株式会社 Nose fairing
CN110530204B (en) * 2019-07-17 2021-10-01 北京玻钢院复合材料有限公司 Directional separating piece and directional separating structure of integrally-broken type launching box sealing cover
US11217872B2 (en) 2020-02-20 2022-01-04 Raytheon Company RF sensor heat shield
CN113173270B (en) * 2021-04-13 2023-04-07 西安航天动力技术研究所 Sectional type piston separating mechanism
US12066276B2 (en) 2022-05-05 2024-08-20 Raytheon Company Sabot or cover for seekers, sensitive windows and surface elements on gun launched munitions
CN120868853B (en) * 2025-09-25 2025-11-25 吉林大学 An automatic opening and closing mechanism for a flow deflector cap

Citations (3)

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Publication number Priority date Publication date Assignee Title
US3485460A (en) * 1968-02-19 1969-12-23 Avco Corp Variable drag ogive
US6142424A (en) * 1995-01-10 2000-11-07 Aerospatiale Societe Nationale Industrielle Method of steering a vehicle and vehicle allowing implementation of the method
US6622971B1 (en) * 2001-05-22 2003-09-23 Lockheed Martin Corporation Adapter for connecting rocket stages

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US3161132A (en) * 1963-01-16 1964-12-15 Cletus J Siebert Epoxy resin structural filler materials
US3601055A (en) * 1969-02-25 1971-08-24 Us Navy Protective nose cover and in-flight removal means
US3960626A (en) * 1971-01-08 1976-06-01 Martin Marietta Corporation Method of making high performance ablative tape
US3970006A (en) * 1975-01-16 1976-07-20 The United States Of America As Represented By The Secretary Of The Air Force Protective cover for a missile nose cone
US4038776A (en) * 1976-06-28 1977-08-02 A. J. Filipeli Co., Inc. Rocket toy
SE8106719L (en) * 1981-11-12 1983-05-13 Foerenade Fabriksverken PROJECTILE
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US5159151A (en) * 1986-05-08 1992-10-27 British Aerospace Public Limited Company Missile nose fairing assembly
US4798143A (en) * 1987-05-06 1989-01-17 Douglas Graham Gas dispensing projectile
US4867357A (en) * 1987-12-21 1989-09-19 General Dynamics Corp., Pomona Division Jettisonable protective cover device
US4949920A (en) * 1989-12-14 1990-08-21 The United States Of America As Represented By The Secretary Of The Navy Ablative cooling of aerodynamically heated radomes
US5494239A (en) * 1994-08-02 1996-02-27 Loral Vought Systems Corporation Expandable ogive
US5824404A (en) * 1995-06-07 1998-10-20 Raytheon Company Hybrid composite articles and missile components, and their fabrication

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3485460A (en) * 1968-02-19 1969-12-23 Avco Corp Variable drag ogive
US6142424A (en) * 1995-01-10 2000-11-07 Aerospatiale Societe Nationale Industrielle Method of steering a vehicle and vehicle allowing implementation of the method
US6622971B1 (en) * 2001-05-22 2003-09-23 Lockheed Martin Corporation Adapter for connecting rocket stages

Also Published As

Publication number Publication date
DE602004008664D1 (en) 2007-10-11
US7082878B2 (en) 2006-08-01
WO2005103600A2 (en) 2005-11-03
EP1685362B1 (en) 2007-08-29
IL173568A0 (en) 2006-07-05
DE602004008664T2 (en) 2008-06-05
IL173568A (en) 2012-02-29
ATE371848T1 (en) 2007-09-15
EP1685362A2 (en) 2006-08-02
JP4444964B2 (en) 2010-03-31
JP2007511730A (en) 2007-05-10
US20050000383A1 (en) 2005-01-06

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