GB1320969A - Missile with fragmenting cover - Google Patents

Missile with fragmenting cover

Info

Publication number
GB1320969A
GB1320969A GB5461370A GB5461370A GB1320969A GB 1320969 A GB1320969 A GB 1320969A GB 5461370 A GB5461370 A GB 5461370A GB 5461370 A GB5461370 A GB 5461370A GB 1320969 A GB1320969 A GB 1320969A
Authority
GB
United Kingdom
Prior art keywords
cover
fragmenting
missile
window
electrical
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
Application number
GB5461370A
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 GB1320969A publication Critical patent/GB1320969A/en
Expired 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)
  • Details Of Aerials (AREA)

Abstract

1320969 Missiles HUGHES AIRCRAFT CO 17 Nov 1970 [23 March 1970] 54613/70 Heading F3A A missile comprises a window 18 through which radiation can pass to a detector, and a protective nose cover 10 which is shattered by means. 28, in response to a control signal, to expose the window. The cover is made. of stressed glass, ceramics or polymeric materials and is externally coated with a material for preventing the build up of electrostatic charges. The fragmenting means comprises a pointed piston propelled by electrical, mechanical or fluid means or by the electrical ignition of a pyrotechnic charge.
GB5461370A 1970-03-23 1970-11-17 Missile with fragmenting cover Expired GB1320969A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US2491370A 1970-03-23 1970-03-23

Publications (1)

Publication Number Publication Date
GB1320969A true GB1320969A (en) 1973-06-20

Family

ID=21823007

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5461370A Expired GB1320969A (en) 1970-03-23 1970-11-17 Missile with fragmenting cover

Country Status (8)

Country Link
US (1) US3674227A (en)
JP (1) JPS5018718B1 (en)
CH (1) CH525798A (en)
DE (1) DE2059492A1 (en)
FR (1) FR2074186A5 (en)
GB (1) GB1320969A (en)
IL (1) IL35596A (en)
SE (1) SE357614B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2129103A (en) * 1982-10-18 1984-05-10 Raytheon Co Mortar round
GB2204668A (en) * 1983-07-16 1988-11-16 Barr & Stroud Ltd Explosion ignition systems
GB2245050A (en) * 1982-09-17 1991-12-18 Short Brothers Ltd Missile fuze
GB2253030A (en) * 1991-02-21 1992-08-26 British Aerospace Missiles
DE10211493B3 (en) * 2002-03-15 2004-02-26 Lfk-Lenkflugkörpersysteme Gmbh Covering cap for a cruise missile comprises a cap held on its edge by a hinge joint and a pull-off fixing which during explosive severing pivots about the movement pole of the hinge joint

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1383513A (en) * 1971-06-10 1974-02-12 Hawker Siddeley Aviation Ltd Aircrew escape systems
JPS49131698U (en) * 1973-03-12 1974-11-12
US4515082A (en) * 1983-09-22 1985-05-07 Ford Aerospace & Communications Corporation Guided projectile lens cover
US4649795A (en) * 1984-05-16 1987-03-17 Hi-Shear Corporation Structural shroud system incorporating a pyrotechnic
US4593637A (en) * 1984-06-04 1986-06-10 The United States Of America As Represented By The Secretary Of The Navy Combination frangible nose cap EMI shield
US4753169A (en) * 1985-12-23 1988-06-28 General Dynamics, Pomona Division Ablating electromagnetic shield sheath
US5159151A (en) * 1986-05-08 1992-10-27 British Aerospace Public Limited Company Missile nose fairing assembly
US4867357A (en) * 1987-12-21 1989-09-19 General Dynamics Corp., Pomona Division Jettisonable protective cover device
US5261629A (en) * 1989-04-08 1993-11-16 Rheinmetall Gmbh Fin stabilized projectile
DE3911576A1 (en) * 1989-04-08 1990-10-11 Rheinmetall Gmbh WING STABILIZED SHELL
GB2250804B (en) * 1990-11-07 1994-06-01 Colebrand Ltd Protective device for a sensing head
US5167386A (en) * 1992-01-21 1992-12-01 Rockwell International Corporation Pyrotechnic removal of a radome cover
DE4235266C1 (en) * 1992-10-20 1993-10-21 Bodenseewerk Geraetetech Connection arrangement for connecting a dome covering a seeker head to the structure of a missile
US5853149A (en) * 1996-04-08 1998-12-29 Raytheon Company Stress-free dome mount missile design
FR2769975B1 (en) * 1997-10-20 2000-01-07 Thomson Csf DEVICE FOR RETAINING IN PARTICULAR THE REAR IGNITER OF A MISSILE
IL139891A (en) * 2000-11-23 2004-07-25 Rafael Armament Dev Authority Jettisonable protective element
FR2840029B1 (en) * 2002-05-27 2004-08-13 Mbdam SHUTTERING SYSTEM FOR A PITCH ORIFICE, ESPECIALLY FOR AN ORIFICE OF AN AIR INPUT ROUTE IN THE COMBUSTION CHAMBER OF A STATOREACTOR
DE10240040A1 (en) * 2002-08-27 2004-03-11 BODENSEEWERK GERäTETECHNIK GMBH Guided missile with detachable protective cap
DE102005030090B4 (en) 2005-06-27 2007-03-22 Diehl Bgt Defence Gmbh & Co. Kg Throw-off hood and missile with detachable hood
US7766277B2 (en) * 2006-01-19 2010-08-03 The Boeing Company Deformable forward pressure bulkhead for an aircraft
EP2002198B1 (en) * 2006-03-30 2013-04-24 Raytheon Company Methods and apparatus for integrated locked thruster mechanism
US8093487B2 (en) * 2008-01-31 2012-01-10 The Penn State Research Foundation Removable protective nose cover
DE102009003201B4 (en) 2009-05-18 2013-07-25 Airbus Operations Gmbh A method of protecting a portion of a surface of an aircraft from contamination by insect debris and / or icing, aircraft having a coating on a portion of its surface, use of a coating, and use of a coating apparatus for coating a portion of a surface of an aircraft with a coating
FR2960055B1 (en) * 2010-05-12 2015-11-20 Tda Armements Sas GUIDED MUNITION PROTECTED BY AERODYNAMIC COIFFE
FR2966919B1 (en) * 2010-10-29 2013-11-01 Tda Armements Sas A SECURE AERODYNAMIC COVER FOR GUIDED MUNITION AND GUIDEED MUNITION COMPRISING SUCH A BOX.
FR2966920B1 (en) * 2010-10-29 2013-05-17 Tda Armements Sas EJECTABLE AERODYNAMIC COIFFE FOR GUIDED MUNITION AND GUIDE MUNITION COMPRISING SUCH A BOX.
US8445823B2 (en) * 2010-11-02 2013-05-21 Raytheon Company Guided munition systems including combustive dome covers and methods for equipping guided munitions with the same
US8461501B2 (en) * 2010-11-02 2013-06-11 Raytheon Company Guided munitions including self-deploying dome covers and methods for equipping guided munitions with the same
US8186260B2 (en) * 2010-11-03 2012-05-29 Raytheon Company Translating adjacent-blast shield and method for protecting external slots of missiles in launcher tubes
US8497456B2 (en) * 2011-03-30 2013-07-30 Raytheon Company Guided munitions including interlocking dome covers and methods for equipping guided munitions with the same
CN111392010B (en) * 2020-04-06 2021-09-17 西北工业大学 Asymmetric buffering head cap for high-speed underwater entry of aircraft
CN111391992A (en) * 2020-04-06 2020-07-10 西北工业大学 High-speed underwater vehicle entering buffering head cap
FR3138203A1 (en) * 2022-07-21 2024-01-26 Safran Electronics & Defense Aerial vehicle with protected frontal optics.

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2245050A (en) * 1982-09-17 1991-12-18 Short Brothers Ltd Missile fuze
GB2245050B (en) * 1982-09-17 1992-05-13 Short Brothers Ltd Missile with proximity fuze
GB2129103A (en) * 1982-10-18 1984-05-10 Raytheon Co Mortar round
GB2204668A (en) * 1983-07-16 1988-11-16 Barr & Stroud Ltd Explosion ignition systems
GB2204668B (en) * 1983-07-16 1989-05-17 Barr & Stroud Ltd Explosion ignition systems
GB2253030A (en) * 1991-02-21 1992-08-26 British Aerospace Missiles
DE10211493B3 (en) * 2002-03-15 2004-02-26 Lfk-Lenkflugkörpersysteme Gmbh Covering cap for a cruise missile comprises a cap held on its edge by a hinge joint and a pull-off fixing which during explosive severing pivots about the movement pole of the hinge joint

Also Published As

Publication number Publication date
SE357614B (en) 1973-07-02
IL35596A0 (en) 1971-04-28
DE2059492A1 (en) 1971-10-07
FR2074186A5 (en) 1971-10-01
CH525798A (en) 1972-07-31
US3674227A (en) 1972-07-04
JPS5018718B1 (en) 1975-07-01
IL35596A (en) 1973-11-28

Similar Documents

Publication Publication Date Title
GB1320969A (en) Missile with fragmenting cover
GB1355862A (en) Missile having a casing and containing secondary projectiles
CA960517A (en) Electrohydraulic plus fuel detonation explosive forming
GB1382888A (en) Tubular cartraidge a launching tube loaded with a cartridge and a method of launching a missile using the loaded launching tube
GB1383512A (en) Detonating cord for aircraft canpoy emergency break-up systems
CA958945A (en) Self-propelling ballistic projectile
GB1262165A (en) Hollow explosive charge missile
GB1426813A (en) Finstabilised projectile
CA993151A (en) Explosive powder driven setting gun with silencing device
FR2287026A1 (en) DETONATOR EXCITABLE BY THE CALORIFIC ENERGY RELEASED BY THE DETONATION OF AN EXPLOSIVE GAS MIXTURE AND DETONATION SYSTEM
GB1371482A (en) Fire-arm ammunition
BR7207038D0 (en) INSTANT MECHANICAL ROCKET FOR ROTATING BAGS WITH DETONATOR AND TRAJECTORY SAFETY
GB1100354A (en) Shaped charge device
GB1516073A (en) Subcalibre projectile
GB1278021A (en) Improvements in or relating to projectiles
BE796200A (en) ROCKET OR PROJECTILE WITH ROCKET CARRYING AN EXPLOSIVE CHARGE
GB1145079A (en) Smoke marker
GB1179458A (en) Bomb adapted to be dropped from an Aircraft
GB1066022A (en) Optical antiflash device
GB1315723A (en) Pyrotechnical illuminating body with light emission
GB1358151A (en) Safety arrangement on an explosive projectile
BE744675A (en) ROCKET ROCKET EQUIPPED WITH A MECHANICAL SAFETY DEVICE FOR HANDLING AND TRAJECTORY OF A PUNCHER FOR EXPLOSIVE HEADS AND WITH ELECTRIC UNDETONATOR FOR HOLLOW-LOAD DRILLING HEADS
GB1248432A (en) Improvements in or relating to seismic charge assemblies for marine exploration purposes
GB1321523A (en) Attaching of a cast explosive charge to the inside of a projectile casing
GB1016585A (en) Improvements in projectiles for practice ammunition

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years