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US2998780A - High velocity, fin stabilized projectile, rifled barrel gun system - Google Patents

  • ️Tue Sep 05 1961

US2998780A - High velocity, fin stabilized projectile, rifled barrel gun system - Google Patents

High velocity, fin stabilized projectile, rifled barrel gun system Download PDF

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Publication number
US2998780A
US2998780A US587910A US58791056A US2998780A US 2998780 A US2998780 A US 2998780A US 587910 A US587910 A US 587910A US 58791056 A US58791056 A US 58791056A US 2998780 A US2998780 A US 2998780A Authority
US
United States
Prior art keywords
sabot
gun
projectile
bore
base
Prior art date
1956-05-28
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 - Lifetime
Application number
US587910A
Inventor
William B Anspacher
Ellis H Scott
Gilbert C Bowen
Joseph J Redmond
Robert L Detwiler
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.)
Individual
Original Assignee
Individual
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.)
1956-05-28
Filing date
1956-05-28
Publication date
1961-09-05
1956-05-28 Application filed by Individual filed Critical Individual
1956-05-28 Priority to US587910A priority Critical patent/US2998780A/en
1961-09-05 Application granted granted Critical
1961-09-05 Publication of US2998780A publication Critical patent/US2998780A/en
1978-09-05 Anticipated expiration legal-status Critical
Status Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F42B14/064Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base

Definitions

  • This invention relates to a sabot for a projectile and more particularly to a sabot for a fin stabilized projectile adapted to withstand rough handling and the action of the gun ramming mechanism as the round is loaded into the gun.
  • a sabot of the present invention possesses all of the advantages of the sabots heretofore devised and none of the foregoing disadvantages.
  • a sabot constructed and arranged to receive and securely hold a fin stabilized projectile therein in such manner that the fins are protected from damage during handling, shipment, and loading of the projectile into the gun, the device also having new and improved means for maintaining the sabot and projectile in a predetermined position within the gun during the ramming operation and for preventing appreciable spin to be imparted thereto during the travel of the sabot through the rifled bore of the gun.
  • One of the objects of the invention is to provide a new and improved sabot for a fin stabilized projectile of subcaliber size from a conventional rifled gun.
  • Another object is to provide a sabot for a sub-caliber fin stabilized projectile whereby the projectile may be fired at high velocity from a conventional rifled gun.
  • Still another object is to provide a sabot for a subcaliber fin stabilized projectile which permits restraint in the gun chamber or bore to position properly during ramming and which does not impart a substantial spin to the projectile as the sabot passes through the bore of the gun.
  • a still further object is to provide a sabot for a fin stabilized projectile for firing from a conventional rifled gun which guides the projectile through the bore of the gun as the gun is fired without imparting rotative movement thereto and which is disengaged from the projectile as the projectile travels beyond the field of the explosive blast.
  • Still another object is to provide a sabot of the character disclosed which will be economical to manufacture, rugged and reliable in operation.
  • FIG. 1 is a view in elevation of the device of the instan invention having a fin stabilized projectile secured thereto;
  • FIG. 2 is an enlarged view in section of the device of FIG. 1 with the projectile removed;
  • FIG. 3 is a plan view of the device of FIG. 2;
  • FIG. 4 is an enlarged view partially in section of the separable bolt structure for clamping the projectile to the base of the sabot.
  • FIG. 1 there is shown thereon a sabot in accordance with a preferred form of the invention indicated generally by numeral 10 and having a projectile 11 provided with a plurality of fin stabilizing elements 12 secured thereto, the projectile being mounted within the sabot and releasably secured thereto.
  • a plurality of longitudinal members 13 are secured to a base 14 as by the plates 15 secured to the base 14 by the bolt 16.
  • each of the longitudinal members or petals 13 is flanged outwardly substantially as shown, the flange portion 17 having a bearing surface for engagement with a complementary conical surface 18 formed on the base 14 and held securely thereagainst by the plate 15.
  • Each of the plates 15 is bolted to the associated petal 13 as by the bolts 19 which pass through the plate 15 and are threaded into the flange portion 17.
  • each of the petals are flared outwardly at an angle, the outwardly flared portions 21 each being provided With an arcuate bearing member 22 or bourrelet secured thereto as by the screws 23 whereby the sabot slides easily within the bore of a conventional rifled gun.
  • Each of the flanged portions 21 is provided with an aperture 24 for release of the gases escaping past the base of the sabot as the gun is fired and thereby reducing the gas pressure between the end portions of the sabot as the gun is fired sufficiently to prevent distortion of the sabot by lateral inward pressure thereof which otherwise might cause the bearing members 22 to bind against the bore of the gun during travel therethrough.
  • annular stop member 25 Threaded exteriorly about the base 14 is an annular stop member 25 having a plurality of circular fin portions 26 formed thereon for engaging the bore of the gun to provide a bearing surface therewith suflicient to prop erly guide the sabot during travel therethrough and to seal the base of the sabot thereto sufficiently to prevent excessive leakage of the propellant gas as the propellant charge is fired.
  • an additional fin portion 27 of greater diameter than the fin portions 26 for engagement with the discontinuous surface at the rear of rifling within the gun thereby to stop the sabot at a predetermined position within the gun and hold it securely during the ramming operation.
  • the stop member 25 is composed of soft metal such, for example, as soft steel whereby the fin portion 27 is sheared as the sabot suddenly moves forward within the gun barrel in response to the explosion of the propellant charge and the sabot, therefore, is thus prevented from being brought into locking engagement with the rifling of the gun whereby the sabot and projectile carried thereby leave the muzzle of the gun with substantial zero spin velocity.
  • the projectile 11 is secured to the base of the sabot by a plurality of shear studs, one end is threaded into a circular cap nut 28 and the other end threaded into the base of the projectile 11, FIG. 4.
  • Each of the studs is composed Of tWO elements 29 and 31 having tapergd flat surfaces secured together at 32 by hard solder, for example, silver solder.
  • the stud is disposed within said annular bore 33 of greater diameter than the stud and terminating at one end thereof in a conical surface 34 abutting a second bore 35 formed within which is disposed a gasket 36 for effecting a seal between the nut and the base 14 as the nut is tightened by a suitable tool.
  • the nut is also provided with a weakened annular portion 37 whereby the central portion of the nut is driven forcibly inward by the explosion of the propellant charge sufficiently to break the soldered joint at 32 and disengage the end portion 29 of the stud from the other end 31 thereof and thereby disengage the means for clamping the projectile to the base of the sabot.
  • the petals or elongated members are composed of metal suitable for the purpose such, for example, as cast aluminum although, if desired, they may be formed from sheet aluminum by a stamping process.
  • the front bearing members 22 may be composed of a single band having weakened portions intermediate each adjacent pair of petals to provide added rigidity to the petal structure during loading of the fin stabilized projectile therein and subsequent handling, the band being weakened sufliciently to cause the band to be severed at each of the weakened portions in response to the pressure of the air within the flared portions 21 thereof as the sabot passes beyond the zone of the explosive blast.
  • a sabot for a fin stabilized projectile having a diameter less than the bore size of a rifled gun from which it is to be fired comprising a circular base plate having an annular bearing surface of circumference slightly less than the bore of the gun, a plurality of longitudinal members individually and coaxially mounted on said base plate in a manner to form a hollow cylinder adapted to receive a projectile, a plurality of metallic arcuate band segments carried by each of said members respectively to form an annular flange on said cylinder, said flange having an outside diameter substantially equal to the bore of the gun from which the projectile is to be fired, and an annular upraised soft metallic lip secured to said base plate and having a diameter slightly greater than the bore of the gun whereby upon firing of the gun said lip is swaged and sheared off thereby allowing the bearing surface to pass slidably within the bore of the gun without locking engagement with the rifling thereof.
  • a sabot for a sub-caliber fin stabilized projectile to be fired from a rifled gun comprising a circular base member, a plurality of elongated guide members, one end of each of said guide members being flanged out- Wardly, means for securing each of said outwardly flanged ends to said base member in annular array, each of said guide members being spaced from the immediately adjacent guide members sutficiently to allow sliding movement of a fin of said projectile, the other end of said guide members being flanged outwardly and provided with an arcuate bearing surface for engagement with the bore of the gun whereby the projectile is maintained in a position coaxial with the bore of the gun as the gun is fired, and means for releasably securing the projectile to the sabot.
  • a sabot according to claim 2 in which the last named means comprises a plurality of shearable studs threaded into the base of the projectile and a plurality of nut members threaded thereon and in engagement with a rear surface of said base, each of said studs comprising a pair of interconnected shearable faces intermediate the ends thereof.
  • each of the cup members comprises an enlarged annular disc having a weakened annular portion arranged coaxial therewith in such manner that the center portion of the nut member is driven inwardly by the force of the explosion sufliciently to shear said studs.
  • each of the flange bearing portions of each of the longitudinal members is provided with an aperture for relieving pressure caused by escape of gases past the base of the sabot as the gun is fired.
  • a sabot for a sub-caliber fin stabilized projectile comprising a circular base member of slightly less diameter than the bore of the gun, an annular bearing member having a plurality of bearing fins circumferentially arranged thereon for sliding movement within the bore of the gun, a circular stop member formed integrally with said annular member and of greater diameter than the bore of the gun for maintaining the sabot in a predetermined position within the gun during a ramming operation, said stop member being composed of soft metal and adapted to be sheared and disengaged from the rifling of the gun as the sabot is moved from said predetermined position by the explosion of the propellant charge within the gun, a plurality of elongated members having flanged e'nds thereon, means for securing said elongated members to the base at one flanged end thereof in circular array in a manner to grip and guide a projectile therein, means for releasably securing the base to the base of the projectile,

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Description

8 7 8 9 0W E 2 F I R E L I A E TJ 6 EMW PT R S1 E E HZ 8 CINZ LU AIGY B a PALM STE SR e ANA IBM BF Sept. 5, 1961 w.

HIGH VELOCITY,

JI JIREDMOND R. L. DETWILER United States Patent 2,998,780 HIGH VELOCITY, FIN STABILIZED PROJECTILE, RIFLED BARREL GUN SYSTEM William B. Anspacher, Ellis H. Scott, and Gilbert C. Bowen, Silver Spring, Joseph J. Redmond, Kensington, and Robert L. Detwiler, Silver Spring, Md., assignors to the United States of America as represented by the Secretary of the Navy Filed May 28, 1956, Ser. No. 587,910 6 Claims. (Cl. 102-93) (Granted under

Title

35, US. Code (1952), sec. 266) The invention described herein may be manufactured and used by or for the Government of the United States of America without the payment of any royalties thereon or therefor.

This invention relates to a sabot for a projectile and more particularly to a sabot for a fin stabilized projectile adapted to withstand rough handling and the action of the gun ramming mechanism as the round is loaded into the gun.

In sabots heretofore devised it has been the usual practice to employ these mechanisms with low velocity smooth bore guns. Such sabots were not suitable for use with subcaliber fin stabilized projectiles whereby the projectiles are fired from conventional rifled guns at high velocity at a zero or low spin as the projectile leaves the muzzle of the gun.

The sabot of the present invention possesses all of the advantages of the sabots heretofore devised and none of the foregoing disadvantages. In accordance with a preferred embodiment of the invention there is provided a sabot constructed and arranged to receive and securely hold a fin stabilized projectile therein in such manner that the fins are protected from damage during handling, shipment, and loading of the projectile into the gun, the device also having new and improved means for maintaining the sabot and projectile in a predetermined position within the gun during the ramming operation and for preventing appreciable spin to be imparted thereto during the travel of the sabot through the rifled bore of the gun.

This desirable result is achieved by the several new and improved features incorporated in the sabot structure, all of which will be more clearly apparent as the description proceeds.

One of the objects of the invention is to provide a new and improved sabot for a fin stabilized projectile of subcaliber size from a conventional rifled gun.

Another object is to provide a sabot for a sub-caliber fin stabilized projectile whereby the projectile may be fired at high velocity from a conventional rifled gun.

Still another object is to provide a sabot for a subcaliber fin stabilized projectile which permits restraint in the gun chamber or bore to position properly during ramming and which does not impart a substantial spin to the projectile as the sabot passes through the bore of the gun.

A still further object is to provide a sabot for a fin stabilized projectile for firing from a conventional rifled gun which guides the projectile through the bore of the gun as the gun is fired without imparting rotative movement thereto and which is disengaged from the projectile as the projectile travels beyond the field of the explosive blast.

Still another object is to provide a sabot of the character disclosed which will be economical to manufacture, rugged and reliable in operation.

Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawing wherein:

FIG. 1 is a view in elevation of the device of the instan invention having a fin stabilized projectile secured thereto;

FIG. 2 is an enlarged view in section of the device of FIG. 1 with the projectile removed;

FIG. 3 is a plan view of the device of FIG. 2; and

FIG. 4 is an enlarged view partially in section of the separable bolt structure for clamping the projectile to the base of the sabot.

Referring now to the drawing on which like numerals of reference are employed to designate like parts throughout the several views and more particularly to FIG. 1 thereof there is shown thereon a sabot in accordance with a preferred form of the invention indicated generally by

numeral

10 and having a

projectile

11 provided with a plurality of fin stabilizing

elements

12 secured thereto, the projectile being mounted within the sabot and releasably secured thereto. A plurality of

longitudinal members

13 are secured to a

base

14 as by the

plates

15 secured to the

base

14 by the

bolt

16. The lower portion of each of the longitudinal members or

petals

13 is flanged outwardly substantially as shown, the flange portion 17 having a bearing surface for engagement with a complementary conical surface 18 formed on the

base

14 and held securely thereagainst by the

plate

15. Each of the

plates

15 is bolted to the associated

petal

13 as by the

bolts

19 which pass through the

plate

15 and are threaded into the flange portion 17. By this arrangement the elongated members or

petals

13 are maintained securely bolted to the base of the sabot in such manner that the upper or forward ends thereof are securely held in mutually spaced adjacency to provide a rigid structure suitable for loading into the gun.

The upper or leading end portion of each of the petals are flared outwardly at an angle, the outwardly flared portions 21 each being provided With an arcuate bearing

member

22 or bourrelet secured thereto as by the

screws

23 whereby the sabot slides easily within the bore of a conventional rifled gun. Each of the flanged portions 21 is provided with an

aperture

24 for release of the gases escaping past the base of the sabot as the gun is fired and thereby reducing the gas pressure between the end portions of the sabot as the gun is fired sufficiently to prevent distortion of the sabot by lateral inward pressure thereof which otherwise might cause the bearing

members

22 to bind against the bore of the gun during travel therethrough.

Threaded exteriorly about the

base

14 is an

annular stop member

25 having a plurality of

circular fin portions

26 formed thereon for engaging the bore of the gun to provide a bearing surface therewith suflicient to prop erly guide the sabot during travel therethrough and to seal the base of the sabot thereto sufficiently to prevent excessive leakage of the propellant gas as the propellant charge is fired. There is also provided on the

stop member

25 an additional

fin portion

27 of greater diameter than the

fin portions

26 for engagement with the discontinuous surface at the rear of rifling within the gun thereby to stop the sabot at a predetermined position within the gun and hold it securely during the ramming operation. The

stop member

25 is composed of soft metal such, for example, as soft steel whereby the

fin portion

27 is sheared as the sabot suddenly moves forward within the gun barrel in response to the explosion of the propellant charge and the sabot, therefore, is thus prevented from being brought into locking engagement with the rifling of the gun whereby the sabot and projectile carried thereby leave the muzzle of the gun with substantial zero spin velocity.

The

projectile

11 is secured to the base of the sabot by a plurality of shear studs, one end is threaded into a

circular cap nut

28 and the other end threaded into the base of the

projectile

11, FIG. 4. Each of the studs is composed Of tWO

elements

29 and 31 having tapergd flat surfaces secured together at 32 by hard solder, for example, silver solder. The stud is disposed within said

annular bore

33 of greater diameter than the stud and terminating at one end thereof in a conical surface 34 abutting a

second bore

35 formed within which is disposed a

gasket

36 for effecting a seal between the nut and the

base

14 as the nut is tightened by a suitable tool. The nut is also provided with a weakened annular portion 37 whereby the central portion of the nut is driven forcibly inward by the explosion of the propellant charge sufficiently to break the soldered joint at 32 and disengage the

end portion

29 of the stud from the

other end

31 thereof and thereby disengage the means for clamping the projectile to the base of the sabot.

As' the sabot and projectile leave the muzzle of the gun and pass beyond the field of the explosive blast, pressure of the air within the interior of the flared portion 21 of the sabot forces the

petals

13 outwardly and simultaneously therewith applies a retardation force to the sabot sufficient for the projectile to be disengaged therefrom in free flight. When this occurs the sabot falls to the ground. The

plates

15 are sufficiently rigid to maintain the

elongated petals

13 in a fixed position during loading of the sabot into the gun. When the sabot has passed beyond the field of the explosive blast, however, the pressure of the air within the flanged portion 21 of the petals causes the petals to be bent outwardly and the projectile to be released therefrom without the application of a drag force on the projectile.

The petals or elongated members are composed of metal suitable for the purpose such, for example, as cast aluminum although, if desired, they may be formed from sheet aluminum by a stamping process. Also, if desired, the

front bearing members

22 may be composed of a single band having weakened portions intermediate each adjacent pair of petals to provide added rigidity to the petal structure during loading of the fin stabilized projectile therein and subsequent handling, the band being weakened sufliciently to cause the band to be severed at each of the weakened portions in response to the pressure of the air within the flared portions 21 thereof as the sabot passes beyond the zone of the explosive blast.

Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.

What is claimed as new and desired to be secured by Letters Patent of the United States is:

We claim:

1. A sabot for a fin stabilized projectile having a diameter less than the bore size of a rifled gun from which it is to be fired, comprising a circular base plate having an annular bearing surface of circumference slightly less than the bore of the gun, a plurality of longitudinal members individually and coaxially mounted on said base plate in a manner to form a hollow cylinder adapted to receive a projectile, a plurality of metallic arcuate band segments carried by each of said members respectively to form an annular flange on said cylinder, said flange having an outside diameter substantially equal to the bore of the gun from which the projectile is to be fired, and an annular upraised soft metallic lip secured to said base plate and having a diameter slightly greater than the bore of the gun whereby upon firing of the gun said lip is swaged and sheared off thereby allowing the bearing surface to pass slidably within the bore of the gun without locking engagement with the rifling thereof.

2. A sabot for a sub-caliber fin stabilized projectile to be fired from a rifled gun comprising a circular base member, a plurality of elongated guide members, one end of each of said guide members being flanged out- Wardly, means for securing each of said outwardly flanged ends to said base member in annular array, each of said guide members being spaced from the immediately adjacent guide members sutficiently to allow sliding movement of a fin of said projectile, the other end of said guide members being flanged outwardly and provided with an arcuate bearing surface for engagement with the bore of the gun whereby the projectile is maintained in a position coaxial with the bore of the gun as the gun is fired, and means for releasably securing the projectile to the sabot.

3. A sabot according to claim 2 in which the last named means comprises a plurality of shearable studs threaded into the base of the projectile and a plurality of nut members threaded thereon and in engagement with a rear surface of said base, each of said studs comprising a pair of interconnected shearable faces intermediate the ends thereof.

4. A sabot in accordance with

claim

3 in which each of the cup members comprises an enlarged annular disc having a weakened annular portion arranged coaxial therewith in such manner that the center portion of the nut member is driven inwardly by the force of the explosion sufliciently to shear said studs.

5. A sabot according to

claim

4 in which each of the flange bearing portions of each of the longitudinal members is provided with an aperture for relieving pressure caused by escape of gases past the base of the sabot as the gun is fired.

6. A sabot for a sub-caliber fin stabilized projectile comprising a circular base member of slightly less diameter than the bore of the gun, an annular bearing member having a plurality of bearing fins circumferentially arranged thereon for sliding movement within the bore of the gun, a circular stop member formed integrally with said annular member and of greater diameter than the bore of the gun for maintaining the sabot in a predetermined position within the gun during a ramming operation, said stop member being composed of soft metal and adapted to be sheared and disengaged from the rifling of the gun as the sabot is moved from said predetermined position by the explosion of the propellant charge within the gun, a plurality of elongated members having flanged e'nds thereon, means for securing said elongated members to the base at one flanged end thereof in circular array in a manner to grip and guide a projectile therein, means for releasably securing the base to the base of the projectile, a bearing surface formed on the outer end portion of each of the other flanged portions of said elongated members for sliding engagement with the bore of the gun, each of said last named flange portions having a cup like interior surface whereby the flanged portions are bent outwardly by air pressure against the cup like surface during free flight of the sabot through the air and the projectile is disengaged therefrom.

References Cited in the file of this patent UNITED STATES PATENTS 2,479,582 McCaslin Aug. 23, 1949 FOREIGN PATENTS 123,501 Great Britain Feb. 27, 1919 584,187 Great Britain Jan. 9, 1947

US587910A 1956-05-28 1956-05-28 High velocity, fin stabilized projectile, rifled barrel gun system Expired - Lifetime US2998780A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3585934A (en) * 1967-11-24 1971-06-22 Aai Corp Underwater ammunition
US3759184A (en) * 1972-01-27 1973-09-18 Us Army Self-obturating, expellable cartridge case
US3805702A (en) * 1972-03-07 1974-04-23 Dynamit Nobel Ag Detachable connection between a projectile and a propellant-charge case
FR2445509A1 (en) * 1978-12-28 1980-07-25 Thomson Brandt LAUNCHING MECHANISM OF A SUB-CALIBER PROJECTILE
US4430942A (en) * 1981-11-05 1984-02-14 The United States Of America As Represented By The Secretary Of The Air Force Missile/canister lateral support pad flyout control system
US4444114A (en) * 1978-08-24 1984-04-24 Rheinmetall Gmbh Munitions round for barrel-type weapons
EP0123299A2 (en) * 1983-04-23 1984-10-31 Rheinmetall GmbH Segmented sabot
US4936219A (en) * 1989-08-10 1990-06-26 The United States Of America As Represented By The Secretary Of The Army Fin protection device
DE19508008A1 (en) * 1995-03-07 1996-09-12 Wegmann & Co Gmbh Launching device for self-propelled missiles, in particular artillery missiles
USH1999H1 (en) * 1999-03-03 2001-11-06 The United States Of America As Represented By The Secretary Of The Army Tuning saboted projectile performance through bourrelet modification
US20030145756A1 (en) * 2002-02-04 2003-08-07 Giat Industries Sabot for fin-stabilised ammunition

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB123501A (en) * 1918-02-12 1919-02-27 John William Rooney Improvements in Shells used in Warfare.
GB584187A (en) * 1941-08-29 1947-01-09 Frantisek Karel Janecek Improvements in or relating to projectiles for firearms
US2479582A (en) * 1945-05-07 1949-08-23 James F Mccaslin Projectile fuse

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB123501A (en) * 1918-02-12 1919-02-27 John William Rooney Improvements in Shells used in Warfare.
GB584187A (en) * 1941-08-29 1947-01-09 Frantisek Karel Janecek Improvements in or relating to projectiles for firearms
US2479582A (en) * 1945-05-07 1949-08-23 James F Mccaslin Projectile fuse

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3585934A (en) * 1967-11-24 1971-06-22 Aai Corp Underwater ammunition
US3759184A (en) * 1972-01-27 1973-09-18 Us Army Self-obturating, expellable cartridge case
US3805702A (en) * 1972-03-07 1974-04-23 Dynamit Nobel Ag Detachable connection between a projectile and a propellant-charge case
US4542696A (en) * 1978-08-24 1985-09-24 Rheinmetall Gmbh Munitions round for barrel-type weapons
US4444114A (en) * 1978-08-24 1984-04-24 Rheinmetall Gmbh Munitions round for barrel-type weapons
US4408538A (en) * 1978-12-28 1983-10-11 Thomson-Brandt Launching mechanism for subcalibre projectile
FR2445509A1 (en) * 1978-12-28 1980-07-25 Thomson Brandt LAUNCHING MECHANISM OF A SUB-CALIBER PROJECTILE
US4430942A (en) * 1981-11-05 1984-02-14 The United States Of America As Represented By The Secretary Of The Air Force Missile/canister lateral support pad flyout control system
EP0123299A2 (en) * 1983-04-23 1984-10-31 Rheinmetall GmbH Segmented sabot
EP0123299A3 (en) * 1983-04-23 1985-01-16 Rheinmetall Gmbh Segmented sabot
US4936219A (en) * 1989-08-10 1990-06-26 The United States Of America As Represented By The Secretary Of The Army Fin protection device
DE19508008A1 (en) * 1995-03-07 1996-09-12 Wegmann & Co Gmbh Launching device for self-propelled missiles, in particular artillery missiles
USH1999H1 (en) * 1999-03-03 2001-11-06 The United States Of America As Represented By The Secretary Of The Army Tuning saboted projectile performance through bourrelet modification
US20030145756A1 (en) * 2002-02-04 2003-08-07 Giat Industries Sabot for fin-stabilised ammunition
US6805058B2 (en) * 2002-02-04 2004-10-19 Giat Industries Sabot for fin-stabilized ammunition

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US3023704A (en) 1962-03-06 Projectiles for mortars and like projectors
US2798433A (en) 1957-07-09 Stable sabot
US2413008A (en) 1946-12-24 Fragmentation bomb
US3107615A (en) 1963-10-22 Non-lethal discarding device
US2992612A (en) 1961-07-18 Projectile