GB1193304A - Projectiles having Means for Correcting the Trajectory - Google Patents

Projectiles having Means for Correcting the Trajectory

Info

Publication number
GB1193304A
GB1193304A GB28551/67A GB2855167A GB1193304A GB 1193304 A GB1193304 A GB 1193304A GB 28551/67 A GB28551/67 A GB 28551/67A GB 2855167 A GB2855167 A GB 2855167A GB 1193304 A GB1193304 A GB 1193304A
Authority
GB
United Kingdom
Prior art keywords
projectile
target
auxiliary
projectiles
reflected
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
GB28551/67A
Inventor
Frederic Edouard Antoine Vyve
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.)
NATIONALE D ARMES DE GEURRE FA
FN Herstal SA
Original Assignee
NATIONALE D ARMES DE GEURRE FA
FN Herstal SA
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 NATIONALE D ARMES DE GEURRE FA, FN Herstal SA filed Critical NATIONALE D ARMES DE GEURRE FA
Publication of GB1193304A publication Critical patent/GB1193304A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F41G7/222—Homing guidance systems for spin-stabilized missiles
    • 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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F41G7/305—Details for spin-stabilized missiles
    • 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
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Landscapes

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

Abstract

1,193,304. Rockets. FABRIQUE NATIONALE D'ARMES DE GUERRE S.A. 21 June, 1967 [4 July, 19661, No. 28551/67. Heading F3A. A projectile 1 whose trajectory is corrected by the lateral ejection of an auxiliary projectile 14 from a diametral housing at or near the centre of gravity of the projectile, comprises a rocket motor 7 for propelling the projectile at a constant velocity during the main part of its flight, profiled stabilization fins 4 for spinning the projectile at a constant period, a propellant charge 13 for the auxiliary projectile, and a firing circuit (not shown) responsive to a means 18 for receiving electromagnetic, infra-red or magnetic waves emitted or reflected by a target, or a laser beam reflected by the target. The projectile includes a hollow charge 9 and a plastics cap 19 opaque to the radiation from the target. In a modification two or more auxiliary projectiles may be used.
GB28551/67A 1966-07-04 1967-06-21 Projectiles having Means for Correcting the Trajectory Expired GB1193304A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE683586 1966-07-04

Publications (1)

Publication Number Publication Date
GB1193304A true GB1193304A (en) 1970-05-28

Family

ID=3849029

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28551/67A Expired GB1193304A (en) 1966-07-04 1967-06-21 Projectiles having Means for Correcting the Trajectory

Country Status (9)

Country Link
US (1) US3398916A (en)
AT (1) AT278594B (en)
BE (1) BE683586A (en)
CH (1) CH469242A (en)
ES (1) ES342471A1 (en)
GB (1) GB1193304A (en)
IL (1) IL28154A (en)
NL (1) NL6708669A (en)
SE (1) SE348829B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE32094E (en) * 1979-11-09 1986-03-25 Avco Corporation Overflying munitions device and system
GB2250804A (en) * 1990-11-07 1992-06-17 Colebrand Ltd Protective device
GB2251834A (en) * 1983-02-22 1992-07-22 George Alexander Tarrant Guided missiles and like devices
GB2334323A (en) * 1983-12-16 1999-08-18 Diehl Gmbh & Co Target-sensing munition
GB2370342A (en) * 1981-11-05 2002-06-26 Emi Ltd Terminally-corrected sub-munition

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2091901B2 (en) * 1970-04-10 1973-12-21 Etu Realisa Electronique
CA1009370A (en) * 1972-01-03 1977-04-26 Ship Systems Laser guided projectile
DE2741984C2 (en) * 1977-09-17 1984-01-26 Franz Rudolf Prof.Dr.Dipl.-Ing. West Vancouver Thomanek Warhead for an anti-tank missile with at least one spiked shaped charge
US4160415A (en) * 1978-05-05 1979-07-10 The United States Of America As Represented By The Secretary Of The Army Target activated projectile
CA1242516A (en) * 1982-04-21 1988-09-27 William H. Bell Terminally guided weapon delivery system
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
DE4210113C1 (en) * 1992-03-27 1998-11-05 Athanassios Dr Ing Zacharias Method of steering flying body for elongated munitions launched from overhead, e.g. from helicopter
US6722609B2 (en) * 1998-02-13 2004-04-20 James M. Linick Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like
WO2000052414A1 (en) * 1999-03-03 2000-09-08 Linick James M Impulse motor to improve trajectory correctable munitions
US6502785B1 (en) * 1999-11-17 2003-01-07 Lockheed Martin Corporation Three axis flap control system
AU2002210130B2 (en) * 2000-05-25 2006-06-08 Metal Storm Limited Directional control of missiles
AUPQ776300A0 (en) * 2000-05-25 2000-08-10 Metal Storm Limited Missile control
US7377468B2 (en) * 2003-08-29 2008-05-27 Smiths Aerospace Llc Active stabilization of a refueling drogue
US6994294B2 (en) * 2003-08-29 2006-02-07 Smiths Aerospace, Inc. Stabilization of a drogue body
US7681839B2 (en) * 2005-02-25 2010-03-23 Smiths Aerospace Llc Optical tracking system for refueling
US8084725B1 (en) * 2008-05-01 2011-12-27 Raytheon Company Methods and apparatus for fast action impulse thruster
RU2443968C2 (en) * 2009-03-19 2012-02-27 Николай Евгеньевич Староверов Anti-helicopter and anti-stealth missile
US10615547B2 (en) 2016-09-08 2020-04-07 Raytheon Company Electrical device with shunt, and receptacle
US10662898B2 (en) 2016-09-08 2020-05-26 Raytheon Company Integrated thruster
CN112199635B (en) * 2020-10-17 2024-03-29 中国人民解放军63876部队 Rocket sled movement trajectory calculation correction method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2029491A (en) * 1934-08-25 1936-02-04 Technicraft Engineering Corp Gun type formation tester
US2258281A (en) * 1938-05-20 1941-10-07 Commercial Ingredients Corp Aerial torpedo
NL228838A (en) * 1957-06-19
US3107617A (en) * 1962-04-11 1963-10-22 William F Loeper Ring decoy launching mechanism

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE32094E (en) * 1979-11-09 1986-03-25 Avco Corporation Overflying munitions device and system
GB2370342A (en) * 1981-11-05 2002-06-26 Emi Ltd Terminally-corrected sub-munition
GB2370342B (en) * 1981-11-05 2002-11-20 Emi Ltd Terminally - corrected sub-munitions
GB2251834A (en) * 1983-02-22 1992-07-22 George Alexander Tarrant Guided missiles and like devices
GB2251834B (en) * 1983-02-22 1992-12-16 George Alexander Tarrant Guided missiles
GB2334323A (en) * 1983-12-16 1999-08-18 Diehl Gmbh & Co Target-sensing munition
GB2334323B (en) * 1983-12-16 1999-12-01 Diehl Gmbh & Co A target-sensing munition
GB2250804A (en) * 1990-11-07 1992-06-17 Colebrand Ltd Protective device
US5187321A (en) * 1990-11-07 1993-02-16 Colebrand Limited Protective device
GB2250804B (en) * 1990-11-07 1994-06-01 Colebrand Ltd Protective device for a sensing head

Also Published As

Publication number Publication date
AT278594B (en) 1970-02-10
CH469242A (en) 1969-02-28
US3398916A (en) 1968-08-27
DE1578139B1 (en) 1971-12-23
BE683586A (en) 1966-12-16
SE348829B (en) 1972-09-11
NL6708669A (en) 1968-01-05
ES342471A1 (en) 1968-07-16
IL28154A (en) 1972-08-30

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees