NO853666L - ARTILLERY PROJECTILY WITH EXTENDED RANGE. - Google Patents

ARTILLERY PROJECTILY WITH EXTENDED RANGE.

Info

Publication number
NO853666L
NO853666L NO853666A NO853666A NO853666L NO 853666 L NO853666 L NO 853666L NO 853666 A NO853666 A NO 853666A NO 853666 A NO853666 A NO 853666A NO 853666 L NO853666 L NO 853666L
Authority
NO
Norway
Prior art keywords
order
projectily
artillery
generating
composition
Prior art date
Application number
NO853666A
Other languages
Norwegian (no)
Other versions
NO158272C (en
NO158272B (en
Inventor
Alain Chevalier
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 NO853666L publication Critical patent/NO853666L/en
Publication of NO158272B publication Critical patent/NO158272B/en
Publication of NO158272C publication Critical patent/NO158272C/en

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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/40Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/12Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Saccharide Compounds (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Air Bags (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Toys (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Abstract

1. An increased-range artillery projectile of any caliber, of the type which comprises at its base (4) a combustion chamber (4a) prolonged by one or more nozzles (12), a pyrotechnic charge (13) generating a base drag reduction, and a charge (14) generating an additional propulsion, characterized in that both charges (13, 14) are integrated into the combustion chamber (4a) and blended at the location of their mating surfaces so as to form a cast cylindrical propellant grain (6) arranged with or without a central channel (9) the composition (13) with a slow burning rate on the order of 0.7 to 2 mm/s under a pressure of 10**5 Pa being primed upon projectile launch in order to initiate at the end of combustion the composition (14) with a quick burning rate on the order of 5 to 20 mm/s under a pressure of 10**6 Pa.
NO853666A 1984-09-19 1985-09-18 ARTILLERY PROJECTLY WITH INCREASED RANGE. NO158272C (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8414332A FR2570485B1 (en) 1984-09-19 1984-09-19 ARTILLERY PROJECT WITH INCREASED RANGE

Publications (3)

Publication Number Publication Date
NO853666L true NO853666L (en) 1986-03-20
NO158272B NO158272B (en) 1988-05-02
NO158272C NO158272C (en) 1988-08-10

Family

ID=9307848

Family Applications (1)

Application Number Title Priority Date Filing Date
NO853666A NO158272C (en) 1984-09-19 1985-09-18 ARTILLERY PROJECTLY WITH INCREASED RANGE.

Country Status (7)

Country Link
EP (1) EP0178959B1 (en)
AT (1) ATE35184T1 (en)
CA (1) CA1298733C (en)
DE (1) DE3563386D1 (en)
ES (1) ES8706941A1 (en)
FR (1) FR2570485B1 (en)
NO (1) NO158272C (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9216295D0 (en) * 1992-07-31 1998-05-06 Secr Defence Long range artillery range

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3217651A (en) * 1960-10-31 1965-11-16 James V Braun Multiple propellent grain for rocket motors
US3260208A (en) * 1962-02-26 1966-07-12 Thiokol Chemical Corp Solid propellant charge for rocket motors
US3283721A (en) * 1964-11-09 1966-11-08 Kruzell George Ralph Reaction type missile
US4213393A (en) * 1977-07-15 1980-07-22 Gunners Nils Erik Gun projectile arranged with a base drag reducing system
FR2522134B1 (en) * 1982-02-23 1986-12-12 France Etat LONG-RANGE ARTILLERY PROJECTILE

Also Published As

Publication number Publication date
CA1298733C (en) 1992-04-14
ES547095A0 (en) 1987-07-01
EP0178959A1 (en) 1986-04-23
EP0178959B1 (en) 1988-06-15
FR2570485B1 (en) 1987-09-11
DE3563386D1 (en) 1988-07-21
FR2570485A1 (en) 1986-03-21
ATE35184T1 (en) 1988-07-15
ES8706941A1 (en) 1987-07-01
NO158272C (en) 1988-08-10
NO158272B (en) 1988-05-02

Similar Documents

Publication Publication Date Title
FR2578044B2 (en) CARBON AMMUNITION, CONSISTING OF A PROJECTILE PROVIDED WITH A STABILIZING EMPENNIAL AND A SOCKET CONTAINING THE PROPULSIVE CHARGE AND AT LEAST PARTIALLY FUEL
ATE344915T1 (en) FIREARMS
ES487280A1 (en) Launching mechanism for subcalibre projectile
GB1510986A (en) Projectile with an ejectable payload
BE874835A (en) ROCKET IN PARTICULAR PYROTECHNICAL ROCKET
FR2343987A1 (en) Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition
GB1465550A (en) Projectile launching device
ATE37950T1 (en) AMMUNITION FOR HUNTING RIFLE.
DE3666101D1 (en) Hollow charge training projectile
ES8309002A1 (en) Gun cartridge for flat trajectory or high angle firing.
AU8293487A (en) Projectile assemblies incorporating discarding sabots
ES449468A1 (en) Assembly for launching a projectile
NO853666L (en) ARTILLERY PROJECTILY WITH EXTENDED RANGE.
ES2143650T3 (en) AMMUNITION FOR WEAPONS OF SMALL, MEDIUM OR THICK CALIBER.
GB1148431A (en) Improvements in or relating to rocket projectiles
GB1074307A (en) Surface igniter for combustible charges
GB1170956A (en) Improvements in or relating to Automatic Weapons for Firing Practice Ammunition.
DE3565426D1 (en) Smoke-producing projectile
AU7969491A (en) Centrally sealed twin launch system
EP0398390A3 (en) Tubular projectiles
FR2390704A1 (en) Self-propelling military projectile - has rocket portion at rear which separates after launching and head which descends vertically onto target
GB1312354A (en) Flying target
IT1231557B (en) Munition sabot booster
GB874499A (en) Improvements in self-propelled projectiles
JPS5446000A (en) Charging for shotgun employing lubricated iron shots