IL88235A0 - Propellant charge for projectile - Google Patents

Propellant charge for projectile

Info

Publication number
IL88235A0
IL88235A0 IL88235A IL8823588A IL88235A0 IL 88235 A0 IL88235 A0 IL 88235A0 IL 88235 A IL88235 A IL 88235A IL 8823588 A IL8823588 A IL 8823588A IL 88235 A0 IL88235 A0 IL 88235A0
Authority
IL
Israel
Prior art keywords
projectile
front part
recess
charge
rear part
Prior art date
Application number
IL88235A
Other versions
IL88235A (en
Original Assignee
France Etat
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 France Etat filed Critical France Etat
Publication of IL88235A0 publication Critical patent/IL88235A0/en
Publication of IL88235A publication Critical patent/IL88235A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/18—Caseless ammunition; Cartridges having combustible cases
    • F42B5/181—Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/067—Mounting or locking missiles in cartridge cases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder

Landscapes

  • General Engineering & Computer Science (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Road Signs Or Road Markings (AREA)
  • Road Paving Structures (AREA)
  • Elimination Of Static Electricity (AREA)
  • Magnetic Heads (AREA)
  • Press Drives And Press Lines (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)

Abstract

The invention relates to a propulsive charge for ammunition comprising a finned projectile (5), consisting of a front part (6) and of a rear part (12), the front part surrounding the fin unit of the projectile (5) and the rear part (12) enclosing an ignition means (4). The rear part (12) is integrated in a case (2) and has a recess (10a), in which the front part (6) is engaged partially or completely in order to ensure that these two parts are fixed together. The recess (10a) is delimited by the case (2) alone or both by the case (2) and by the rear part (12) of the charge. The front part (6) is integrated in a housing (7) fitted on the projectile (5) and closed by means of a cover (8) having vents (11), said housing being fitted into the recess (10a) and forming a means for connecting the front part (6) of the charge to the projectile (5). The invention is used for ammunition of the finned arrow type. <IMAGE>
IL88235A 1987-10-29 1988-10-30 Propellant charge for projectile IL88235A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8714975A FR2622687B1 (en) 1987-10-29 1987-10-29 PROPULSIVE LOADING FOR AMMUNITION COMPRISING A POINTED PROJECTILE AND ITS MANUFACTURING METHOD

Publications (2)

Publication Number Publication Date
IL88235A0 true IL88235A0 (en) 1989-06-30
IL88235A IL88235A (en) 1993-02-21

Family

ID=9356283

Family Applications (1)

Application Number Title Priority Date Filing Date
IL88235A IL88235A (en) 1987-10-29 1988-10-30 Propellant charge for projectile

Country Status (7)

Country Link
EP (1) EP0314547B1 (en)
AT (1) ATE102704T1 (en)
CA (1) CA1331315C (en)
DE (1) DE3888288T2 (en)
ES (1) ES2051878T3 (en)
FR (1) FR2622687B1 (en)
IL (1) IL88235A (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5179250A (en) * 1989-10-19 1993-01-12 Olin Corporation Segmented cartridge assembly
DE4020691A1 (en) * 1990-06-29 1992-01-02 Dynamit Nobel Ag WING STABILIZED SHELL
DE4041611C2 (en) * 1990-12-22 1997-11-27 Rheinmetall Ind Ag Split ammunition
US5353710A (en) * 1991-02-11 1994-10-11 Giat Industries Container fitted with electrical connecting means
FR2672674B1 (en) * 1991-02-11 1995-01-13 Giat Ind Sa CONTAINER PROVIDED WITH ELECTRICAL CONNECTION MEANS.
DE4138269C2 (en) * 1991-11-21 1998-01-15 Rheinmetall Ind Ag ammunition
FR2710975B1 (en) * 1993-10-04 1995-12-08 Giat Ind Sa Artillery ammunition element and ammunition obtained by assembling a plurality of such elements.
FR2763392B1 (en) 1997-05-15 1999-06-11 Giat Ind Sa BOX FOR PROPULSIVE CHARGE
DE19950002A1 (en) * 1999-10-15 2001-04-19 Diehl Stiftung & Co Projectile acceleration device
FR2806789B1 (en) 2000-03-23 2002-06-07 Giat Ind Sa IGNITION TUBE FOR ARTILLERY AMMUNITION
DE10055068B4 (en) * 2000-11-07 2006-08-17 Rheinmetall Waffe Munition Gmbh cartridge
FR2849179B1 (en) 2002-12-18 2006-06-30 Giat Ind Sa MUNITION WITHOUT SLEEVE AND METHOD FOR MOUNTING SUCH AMMUNITION
FR2869101B1 (en) 2004-04-15 2006-06-02 Giat Ind Sa MUNITION WITHOUT SLEEVE AND METHOD FOR MOUNTING SUCH AMMUNITION
FR2888924B1 (en) 2005-07-25 2007-08-24 Giat Ind Sa METHOD OF MOUNTING MUNITION

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2323244C3 (en) * 1973-05-09 1979-04-19 Rheinmetall Gmbh, 4000 Duesseldorf Wing-stabilized sub-caliber bullet
FR2343987A1 (en) * 1976-03-08 1977-10-07 France Etat Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition
DE3309288A1 (en) * 1983-03-16 1984-09-20 Diehl GmbH & Co, 8500 Nürnberg SLEEVELESS AMMUNITION FOR MACHINE ARMS
FR2587329B1 (en) * 1985-09-19 1989-05-12 Poudres & Explosifs Ste Nale BINDING-FILLER ADHESION AND PROPULSIVE COMPOSITION CONTAINING THE SAME

Also Published As

Publication number Publication date
CA1331315C (en) 1994-08-09
FR2622687A1 (en) 1989-05-05
FR2622687B1 (en) 1993-05-28
DE3888288D1 (en) 1994-04-14
EP0314547B1 (en) 1994-03-09
ES2051878T3 (en) 1994-07-01
IL88235A (en) 1993-02-21
EP0314547A1 (en) 1989-05-03
ATE102704T1 (en) 1994-03-15
DE3888288T2 (en) 1994-08-04

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