AU2822484A - Sabot projectile - Google Patents

Sabot projectile

Info

Publication number
AU2822484A
AU2822484A AU28224/84A AU2822484A AU2822484A AU 2822484 A AU2822484 A AU 2822484A AU 28224/84 A AU28224/84 A AU 28224/84A AU 2822484 A AU2822484 A AU 2822484A AU 2822484 A AU2822484 A AU 2822484A
Authority
AU
Australia
Prior art keywords
projectile
sabot projectile
flow range
speed flow
separation
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.)
Granted
Application number
AU28224/84A
Other versions
AU557827B2 (en
Inventor
Hansjoerg Becker
Jurgen Bocker
Gerhard Glotz
Jurgen Leeker
Patrick Montier
Jean-Claude Sauvestre
Walter Simon
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.)
Rheinmetall Industrie AG
Direction General pour lArmement DGA
Original Assignee
Etat Francais Le Delegue General Pour Larmement
Rheinmetall GmbH
Direction General pour lArmement DGA
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 Etat Francais Le Delegue General Pour Larmement, Rheinmetall GmbH, Direction General pour lArmement DGA filed Critical Etat Francais Le Delegue General Pour Larmement
Publication of AU2822484A publication Critical patent/AU2822484A/en
Application granted granted Critical
Publication of AU557827B2 publication Critical patent/AU557827B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/24Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction with grooves, recesses or other wall weakenings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/06Sub-calibre projectiles having sabots; Sabots therefor
    • F42B14/061Sabots for long rod fin stabilised kinetic energy projectiles, i.e. multisegment sabots attached midway on the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)
  • Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Saccharide Compounds (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Memory System Of A Hierarchy Structure (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Nitrogen And Oxygen As The Only Ring Hetero Atoms (AREA)
  • Toys (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Tires In General (AREA)
  • Other Air-Conditioning Systems (AREA)
  • Steroid Compounds (AREA)

Abstract

The point portion (15) of a reduced calibre projectile (10) has a discontinuous contour in the form of a circular groove (20). Thereby, a boundary layer is determined between a supersonic speed flow range and a subsonic speed flow range; thereby it is possible to eliminate perturbations due to the flow during the separation of the sabot segments, not shown, of the projectile (10).
AU28224/84A 1983-04-23 1984-04-18 Sabot projectile Ceased AU557827B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19833314750 DE3314750A1 (en) 1983-04-23 1983-04-23 AGENT FOR IMPROVING THE RELEASE BEHAVIOR OF DRIVING CAGE SEGMENTS FROM A RIFLE BULLET FOR THE PIPE ARM
DE3314750 1983-04-23

Publications (2)

Publication Number Publication Date
AU2822484A true AU2822484A (en) 1984-11-19
AU557827B2 AU557827B2 (en) 1987-01-08

Family

ID=6197165

Family Applications (1)

Application Number Title Priority Date Filing Date
AU28224/84A Ceased AU557827B2 (en) 1983-04-23 1984-04-18 Sabot projectile

Country Status (14)

Country Link
EP (1) EP0123266B1 (en)
JP (1) JPS61500076A (en)
KR (1) KR850000664A (en)
AT (1) ATE30081T1 (en)
AU (1) AU557827B2 (en)
BR (1) BR8406813A (en)
DE (2) DE3314750A1 (en)
DK (1) DK155857C (en)
ES (1) ES287013Y (en)
GR (1) GR81472B (en)
IN (1) IN161067B (en)
PT (1) PT78472B (en)
TR (1) TR22229A (en)
WO (1) WO1984004380A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU685027B2 (en) * 1995-06-07 1998-01-08 Raytheon Company Gyroscopically stabilized projectile system for use against underwater objects

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241309B (en) * 1986-02-20 1992-02-05 Royal Ordnance Plc Projectiles and components therefor
DE4007103A1 (en) * 1990-03-07 1991-09-12 Rheinmetall Gmbh Sabot for sub-calibre projectile
DE4022462A1 (en) * 1990-07-14 1992-01-16 Diehl Gmbh & Co Solid air-launched underwater projectile - has core with shortened front protected by ballistic cap
JPH10501883A (en) * 1995-06-07 1998-02-17 エイチイー・ホールディングス・インコーポレーテッド・ドゥーイング・ビジネス・アズ・ヒューズ・エレクトロニクス Full caliber bullet for use against underwater targets
IL120159A (en) * 1995-06-07 2000-11-21 Raytheon Co Aerodynamically stabilized projectile system for use against under water objects

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR454822A (en) * 1912-09-26 1913-07-16 Robert Abbott Hadfield Breast Piercing Projectile Hats Improvements
FR493570A (en) * 1916-10-16 1919-08-13 Bento Caeiro Method and device for increasing the range of projectiles
US2373883A (en) * 1942-10-30 1945-04-17 Clyde B Ferrel Shell structure
FR1206606A (en) * 1951-11-07 1960-02-10 Tech De Rech S Ind & Mecanique Fletched projectile
US3672304A (en) * 1970-03-30 1972-06-27 Lockheed Aircraft Corp Special purpose firearms projectile
DE2323244C3 (en) * 1973-05-09 1979-04-19 Rheinmetall Gmbh, 4000 Duesseldorf Wing-stabilized sub-caliber bullet
US4405100A (en) * 1981-02-20 1983-09-20 The United States Of America As Represented By The Secretary Of The Navy Turbulence generator for maximizing configuration tolerances of free flight ordnance
SE444983B (en) * 1981-09-09 1986-05-20 Bofors Ab OVEN ENDAMAL EXTENSIBLE WINDOW STABILIZED AMMUNITION UNIT

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU685027B2 (en) * 1995-06-07 1998-01-08 Raytheon Company Gyroscopically stabilized projectile system for use against underwater objects

Also Published As

Publication number Publication date
AU557827B2 (en) 1987-01-08
JPS61500076A (en) 1986-01-16
PT78472A (en) 1984-05-01
DE3314750A1 (en) 1984-10-25
WO1984004380A1 (en) 1984-11-08
ES287013Y (en) 1986-06-16
DK155857C (en) 1989-10-02
EP0123266A1 (en) 1984-10-31
DK544884A (en) 1984-11-15
ATE30081T1 (en) 1987-10-15
PT78472B (en) 1986-03-20
DE3466593D1 (en) 1987-11-05
TR22229A (en) 1986-10-09
DK544884D0 (en) 1984-11-15
KR850000664A (en) 1985-02-28
EP0123266B1 (en) 1987-09-30
GR81472B (en) 1984-12-11
ES287013U (en) 1985-11-16
BR8406813A (en) 1985-03-19
IN161067B (en) 1987-09-26
DK155857B (en) 1989-05-22

Similar Documents

Publication Publication Date Title
DE3261740D1 (en) Stage of a gas turbine jet engine with air cooling means for the turbine rotor disc
IT8319318A0 (en) SYSTEM FOR REGULATING THE SPEED OF AN ENGINE.
JPS538855A (en) Condensing heat transmission wall
DE3273111D1 (en) Method and arrangement for the continuous running speed control of brushless d.c.motors
FR2521639B1 (en) HIGH PERFORMANCE PROPELLER PROPULSION ENGINE
DE3860591D1 (en) CENTRIFUGAL COMPRESSOR WITH AERODYNAMIC VARIABLE DIFFUSER GEOMETRY.
AU560074B2 (en) Missile with gas jets
CA1004479A (en) Jet propulsion engine for subsonic and supersonic speeds
AU557827B2 (en) Sabot projectile
GB2070139B (en) Inlet cowl for supersonic aircraft engine
ES8707607A1 (en) Propulsion means for reducing the base drag.
CA2046033A1 (en) Aircraft pitch and thrust control system
EP0398839A3 (en) Helicopter control with multiple schedule rotor speed decay anticipator
FR2582798B1 (en) PROXIMITY ROCKET FOR ARTILLERY PROJECTILE OF THE TYPE WITH REDUCTION OF AERODYNAMIC PULL TRAIL
IT8423422A0 (en) SETTING SYSTEM FOR GUIDED AIRCRAFT, FLYING AT SUPERSONIC SPEED.
JPS5353832A (en) Method and apparatus for constant speed running of vehicles
FI921294A (en) FOERFARANDE OCH ANORDNING FOER TRYCKUTJAEMNING I SLANGAR VID SPRUTNING AV TVAO KOMPONENTER.
EP0371505A3 (en) Linear driving apparatus
GB8509970D0 (en) Engine speed regulating system
JPS5738271A (en) System for controlling winder with taping function
JPS5311257A (en) Total flow turbine
SU1066265A1 (en) Low-pressure gas-turbine engine system of controlling speed of rotor rotation
EP0092869A3 (en) Improved motor
Petrakov Refining of High Speed Profile Machining Processes
JPS5373668A (en) Foreign matter sepapator