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GB1554098A - Tubular projectile - Google Patents

Tubular projectile

Info

Publication number
GB1554098A
GB1554098A GB49862/77A GB4986277A GB1554098A GB 1554098 A GB1554098 A GB 1554098A GB 49862/77 A GB49862/77 A GB 49862/77A GB 4986277 A GB4986277 A GB 4986277A GB 1554098 A GB1554098 A GB 1554098A
Authority
GB
United Kingdom
Prior art keywords
projectile
ratio
passage cross
tubular body
constricted region
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
GB49862/77A
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.)
CA MINISTER NAT DEFENCE
Minister of National Defence of Canada
Original Assignee
CA MINISTER NAT DEFENCE
Minister of National Defence of Canada
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 CA MINISTER NAT DEFENCE, Minister of National Defence of Canada filed Critical CA MINISTER NAT DEFENCE
Publication of GB1554098A publication Critical patent/GB1554098A/en
Expired 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/34Tubular projectiles

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Paper (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The projectile consists of a tubular body (10), of a cap (16) which breaks at the start of the shot, a delivery casing (14) which detaches at the exit of the gun, and a forcing belt (12). At the front end, the internal and external surfaces of the body (10) are conical and delimit a leading edge whose angle is between 5 DEG and 15 DEG . The passage cross-section inside the body decreases from the front towards a cylindrical constricted region, the ratio between these passage cross-sections in the constricted region and at the entry being at least 0.65, but less than 1, and the ratio between the maximum wall thickness and the half-calibre of the projectile being between 0.18 and 0.45. The conditions of flow in the tubular body are such that the drag is low in a first part of the trajectory, but increases sharply when the Mach number has fallen to a particular value, which makes the projectile particularly useful as a training projectile. <IMAGE>
GB49862/77A 1976-12-01 1977-11-30 Tubular projectile Expired GB1554098A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US74682076A 1976-12-01 1976-12-01

Publications (1)

Publication Number Publication Date
GB1554098A true GB1554098A (en) 1979-10-17

Family

ID=25002475

Family Applications (1)

Application Number Title Priority Date Filing Date
GB49862/77A Expired GB1554098A (en) 1976-12-01 1977-11-30 Tubular projectile

Country Status (10)

Country Link
JP (1) JPS53118900A (en)
BE (1) BE861230A (en)
BR (1) BR7707970A (en)
CA (1) CA1064321A (en)
CH (1) CH623407A5 (en)
DE (1) DE2753633A1 (en)
FR (1) FR2373033A1 (en)
GB (1) GB1554098A (en)
IN (1) IN148611B (en)
SE (1) SE432831B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2130691A (en) * 1982-11-24 1984-06-06 Mauser Werke Oberndorf Projectile with a tubular body

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL51505A (en) * 1976-03-26 1983-10-31 Flatau Abraham Supersonic low drag tubular projectile
DE3335997A1 (en) * 1983-10-04 1985-04-11 Rheinmetall GmbH, 4000 Düsseldorf TRAINING FLOOR
JPH0717999Y2 (en) * 1988-11-30 1995-04-26 防衛庁技術研究本部長 Training bullets

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR427714A (en) * 1911-03-24 1911-08-11 Haralambi Djamdjieff Hollow projectile system
DE1453827A1 (en) * 1965-05-29 1969-10-23
CA956179A (en) * 1971-06-17 1974-10-15 Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government Tubular projectile
AU7519774A (en) * 1973-11-16 1976-05-13 Ca Minister Nat Defence Tubular projectile
IL51505A (en) * 1976-03-26 1983-10-31 Flatau Abraham Supersonic low drag tubular projectile

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2130691A (en) * 1982-11-24 1984-06-06 Mauser Werke Oberndorf Projectile with a tubular body

Also Published As

Publication number Publication date
IN148611B (en) 1981-04-18
CA1064321A (en) 1979-10-16
FR2373033A1 (en) 1978-06-30
SE432831B (en) 1984-04-16
BE861230A (en) 1978-03-16
DE2753633A1 (en) 1978-06-08
CH623407A5 (en) 1981-05-29
JPS53118900A (en) 1978-10-17
BR7707970A (en) 1978-08-15
SE7713657L (en) 1978-06-02

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee