GB1284666A - Improvements relating to projectiles - Google Patents

Improvements relating to projectiles

Info

Publication number
GB1284666A
GB1284666A GB4248570A GB4248570A GB1284666A GB 1284666 A GB1284666 A GB 1284666A GB 4248570 A GB4248570 A GB 4248570A GB 4248570 A GB4248570 A GB 4248570A GB 1284666 A GB1284666 A GB 1284666A
Authority
GB
United Kingdom
Prior art keywords
projectile
sticks
tube
propellant
tail
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
GB4248570A
Inventor
Bjarne Narvesen
Edvard Troen
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.)
Raufoss Ammunisjonsfabrikker AS
Original Assignee
Raufoss Ammunisjonsfabrikker AS
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
Priority to NL7013071A priority Critical patent/NL149906B/en
Application filed by Raufoss Ammunisjonsfabrikker AS filed Critical Raufoss Ammunisjonsfabrikker AS
Priority to GB4248570A priority patent/GB1284666A/en
Priority to AU19858/70A priority patent/AU452172B2/en
Publication of GB1284666A publication Critical patent/GB1284666A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/02Cartridges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/02Cartridges
    • F42B8/10Cartridges with sub-calibre adaptor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/12Projectiles or missiles
    • F42B8/24Rockets

Abstract

1284666 Projectile and launcher; rocket launcher RAUFOSS AMMUNISJONSFAB RIKKER AS 4 Sept 1970 42485/70 Headings F3A and F3C [Also in Division F1] A projectile for use in a sub-calibre, antitank, training weapon comprises a plurality of propellant sticks 4 arranged around a rod 2, and an igniter 10 for the propellant sticks contained within a tail piece 3 which serves both as a nozzle and a stabilizing fin. A central hub 7 is connected to a cylindrical part 6 of the tail-piece by means of an apertured web 8 and contains a tracer charge. The igniting composiposition 16 extends along a flexible tube 14 to a primer 15. In use, the projectile is placed in a sub-calibre launching tube 21 in the weapon 20, and the primer 15 is located within percussion firing means 23. Whilst the projectile is within the launching tube the wall of the tube serves as a rocket motor casing and the propellant gases from the ignited sticks 4 pass rearwardy through the tail piece 3 once sufficient pressure has been developed to eject the spent igniter 10 therefrom.
GB4248570A 1970-09-03 1970-09-04 Improvements relating to projectiles Expired GB1284666A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
NL7013071A NL149906B (en) 1970-09-03 1970-09-03 ROCKET SHIP.
GB4248570A GB1284666A (en) 1970-09-03 1970-09-04 Improvements relating to projectiles
AU19858/70A AU452172B2 (en) 1970-09-03 1970-09-11 Improvements relating to projectiles

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL7013071A NL149906B (en) 1970-09-03 1970-09-03 ROCKET SHIP.
GB4248570A GB1284666A (en) 1970-09-03 1970-09-04 Improvements relating to projectiles
AU19858/70A AU452172B2 (en) 1970-09-03 1970-09-11 Improvements relating to projectiles

Publications (1)

Publication Number Publication Date
GB1284666A true GB1284666A (en) 1972-08-09

Family

ID=27152538

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4248570A Expired GB1284666A (en) 1970-09-03 1970-09-04 Improvements relating to projectiles

Country Status (3)

Country Link
AU (1) AU452172B2 (en)
GB (1) GB1284666A (en)
NL (1) NL149906B (en)

Also Published As

Publication number Publication date
AU452172B2 (en) 1974-08-14
NL149906B (en) 1976-06-15
NL7013071A (en) 1972-03-07
AU1985870A (en) 1972-03-19

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Legal Events

Date Code Title Description
PS Patent sealed
PE20 Patent expired after termination of 20 years