US2913960A - Light weight t-20 shoulder stock for 3.5 inch rocket launcher - Google Patents
Light weight t-20 shoulder stock for 3.5 inch rocket launcher Download PDFInfo
- Publication number
- US2913960A US2913960A US570196A US57019656A US2913960A US 2913960 A US2913960 A US 2913960A US 570196 A US570196 A US 570196A US 57019656 A US57019656 A US 57019656A US 2913960 A US2913960 A US 2913960A
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- US
- United States
- Prior art keywords
- launcher
- shoulder
- shoulder stock
- light weight
- stock
- 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 - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/045—Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
- F41F3/0455—Bazookas
Definitions
- This invention relates to an interchangeable ground and shoulder mount for rocket launchers.
- Launchers used in mounts of this type are usually those of the M20 or M2031, 3.5 inch class. They may employ a forward bipodsection and a rearward section consisting of a combined legand shoulder stock. In order to use the launcher upon the shoulder, the forward bipod must'be folded into stowed position. Hence the launcher carries the added weight of the bipod at all times. With the present invention, the launcher may be quickly dismounted from the tripod and with a minimum of' manipulation can be converted into a mobile lightweight'launcher to be fired from the shoulder of the gunner.-
- an important object of this invention is to provide a ground mount of three sections, quickly dismounted and of lightweight construction throughout.
- Anotherobject of the invention is to provide a mounting mechanismthat will provide precise yet rapid controlled adjustment in elevation and free traverse in azimuth.
- a further object of the invention is to provide a launcher mounting mechanism permitting the launcher to be readily converted from a ground mounted fieldpiece to a mobile shoulder-supported mount.
- a still further object of the invention is to provide a mount to be used with existing tripods for launchers of this type.
- Figure 1 is a side elevation of a launcher mounted for shoulder firing and illustrates the shoulder stock.
- Figure 2 is a sectional view taken along the line 2-2 on Figure 1 looking in the direction of the arrows.
- Figure 3 is a partial perspective view of the ends of the shoulder stock showing clamp members attached thereto.
- Figure 4 is a perspective view showing a launcher mounted upon the cradle section and also mounted upon a tripod for firing from a prone or sitting position, the shoulder stock section being in stowed position.
- Figure 5 is a perspective view of the shoulder stock mounted upon the firing position clips that are mounted in the mounting bands.
- Figure 6 is a sectional view taken along lines 6-6 on Figure 5 and looking in the direction of the arrows, showing the mounting band adjusting means.
- Figure 7 is a side elevation, partly broken away, illustrating the cradle member and elevational adjustment of the same.
- Figure 8 is a fragmentary front view of the cradle and
- Figure 9 is a top plan view of the cradle.
- 1 indi cates generally a tripod of either the M77 or M1917 tion between the frame and yoke.
- mount class and consisting of ground engaging legs 2 adjustably mounted to a pintle socket member 3.
- 4 indicates generally a cradle section, comprising a yoke member 5 pivotally mounted by a nut and a bolt 6 to a pintle frame section 7.
- Belleville spring washers 8, Figure 8 between the frame 7 and yoke 5 provides fric- Elevational control of the yoke 5 is obtained by turning a hand wheel 9 mounted at one end of an elongated shaft 10 journaled in bearings 11 integrally mounted from the lower surface of yoke 5.
- a worm 12 is fixed on the other end of shaft 10 and meshes with a pair of arcuate internal gear segments 13 fixed to the floor of the frame 7.
- a pintle 16 is attached to the under face of frame 7 by bolts 15 and is adapted to fit within the pintle socket member 3 of the tripod 1 whereby the frame and parts supported thereby may be trained as a unit in azimuth.
- Forward and rearward mounting lugs 17 and 18 are formed integrally on the respective ends of the upper surface of yoke member 5 for mounting forward and rearward launcher tube mounting bands 19 and 20 respectively, by pins 21 and 22. These bands are adapted to receive the launcher tube 23.
- the bands 19 and 20 are similar in construction and consist of afiexible strap adapted to surroundthe tube of the launcher.
- each band is formed with an adjustable connection whereby its effective length may be varied to contract the same about the launcher tube.
- one end of each strap is split and the two parts thus formed are rolled or looped as at 2311 to rotatably receive the ends of a draw pin 23b.
- the mid portion of this pin is transversely drilled to rotatably accommodate a screw 24a whose threaded end engages a tapped hole in the other and thickened end 24 of the strap.
- each band may be contracted about the tube by turning of screw 24a.
- each strap has a tapered undercut lug or bracket 25 secured, as by welding, to its lower surface.
- Each lug forms a portion of a bayonet joint for a purpose subsequently explained.
- Similar tapered lugs 26 are provided upon the upper and outer side of the bands 19 and 20.
- Spaced depending apertured ears or lugs 27 are provided on each of the bands 19 and 29 on respective sides of the lug 25 for mounting the bands on the yoke member 5. This mounting is effected by pins 21 and 22 which pass through the respective pairs of depending ears and the upstanding lugs 17 and 18 on yoke member 5, received between them.
- the lugs 25 and 26 are adapted to receive tapered clips 29 and 30 respectively, fixed to the ends of a shoulder stock 28.
- the shape and construction of this guard are obvious from inspection of Figures 1, 4 and 5.
- Figure 4 shows the guard attached to lugs 26 while Figures 1 and 5 show it attached to lugs 25.
- bands 19 and 20 are placed about the tube and clamped thereto by turning the screws 24a.
- the bands are then attached to the cradle section by the pins 21 and 22, and the assembly is mounted to the tripod 1 by insertion of the pintle 16 into the pintle socket 3 of same.
- the shoulder stock 28 is mounted upon lugs 26 by its clips 29 and 30 whereby it is secured in the position shown upon Figure 4.
- the launcher is now in position for firing from prone or sitting position.
- the mountin'g bands 19 and 20 are disengaged by' removing pins 21 and 22 and lifting the launcher from the cradle.
- a pair of split rings encircling said tube, in axially spaced relation therealong, each said ring terminating at one of their ends thereof in a pair of spaced loops and at their other ends in a thickened portion
- means for tightening said rings about said tube comprising a draw pin rotatably'mounted in said loops, a screw transversely piercing said draw pins at a medial point and loops, each said screw to" be received” in a threaded hole being disposed between said in each said thickened portion, a tapered bracket secured to the underside of each said ring and a shoulder stock having a tapered clip secured to its respective ends adapted to'fit a respectiye hraeket on said rings, said brackets and said clipsltapering inopposite directions whereby theflresiliency of said stock. releasably' retains said stock on'a pair of said brackets;
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
Nov. 24, 1959 H. HARVEY ETAL 2,913,960
LIGHT WEIGHT T-20 SHOULDER s'rocx FOR 3.5 men ROCKET LAUNCHER Filed March 7, 1956 s Sheets-Sheet 1 JNVEN TORs, HErbEr' c Harvey BY Ecephan Afiisam.
.AITURNEYS.
1959 H. HARVEY ET AL LIGHT WEIGHT T-2O SHOULDER STOCK FOR 3.5 INCH ROCKET LAUNCHER 3 Sheets-Sheet 2 Filed March 7, 1956 INVENTOR Herher liar-veg 51: Epharl A E fl;am
ATTORNEYS.
Nov. 24, 1959 H. HARVEY ETAL LIGHT WEIGHT T-2O SHOULDER STOCK FOR 3.5 INCH ROCKET LAUNCHER FiledMarch 7, 1956 5 Sheets-Sheet 3 IN V EN TORS Her'harl: Han-veg BY 5: ephen .A. 51 am United Sta Patent 9 LIGHT WEIGHT T-20 SHOULDER STOCK FOR 3.5
' INCH ROCKET LAUNCHER Herbert Harvey, Redondo Beach, and Stephen A. Stam, Glendale, Calif., assignors, by mesne assignments, to the United States of America as represented by the Secretary of the Army Application March 7, 1956, Serial No. 570,196
2 Claims. (Cl. 891.7)
This invention relates to an interchangeable ground and shoulder mount for rocket launchers.
Launchers used in mounts of this type are usually those of the M20 or M2031, 3.5 inch class. They may employ a forward bipodsection and a rearward section consisting of a combined legand shoulder stock. In order to use the launcher upon the shoulder, the forward bipod must'be folded into stowed position. Hence the launcher carries the added weight of the bipod at all times. With the present invention, the launcher may be quickly dismounted from the tripod and with a minimum of' manipulation can be converted into a mobile lightweight'launcher to be fired from the shoulder of the gunner.-
'Hence, an important object of this invention is to provide a ground mount of three sections, quickly dismounted and of lightweight construction throughout.
Anotherobject of the invention is to provide a mounting mechanismthat will provide precise yet rapid controlled adjustment in elevation and free traverse in azimuth. i
A further object of the invention is to provide a launcher mounting mechanism permitting the launcher to be readily converted from a ground mounted fieldpiece to a mobile shoulder-supported mount.
A still further object of the invention is to provide a mount to be used with existing tripods for launchers of this type.
Other objects and advantages of the invention will become apparent during the course of the following description:
In the accompanying drawings, forming a part of this specification, and in which like numerals are employed to designate like parts throughout the same:
Figure 1 is a side elevation of a launcher mounted for shoulder firing and illustrates the shoulder stock.
Figure 2 is a sectional view taken along the line 2-2 on Figure 1 looking in the direction of the arrows.
Figure 3 is a partial perspective view of the ends of the shoulder stock showing clamp members attached thereto.
Figure 4 is a perspective view showing a launcher mounted upon the cradle section and also mounted upon a tripod for firing from a prone or sitting position, the shoulder stock section being in stowed position.
Figure 5 is a perspective view of the shoulder stock mounted upon the firing position clips that are mounted in the mounting bands.
Figure 6 is a sectional view taken along lines 6-6 on Figure 5 and looking in the direction of the arrows, showing the mounting band adjusting means.
Figure 7 is a side elevation, partly broken away, illustrating the cradle member and elevational adjustment of the same.
Figure 8 is a fragmentary front view of the cradle and,
Figure 9 is a top plan view of the cradle.
In the drawing, wherein for the purpose of illustration is shown a preferred embodiment of the invention, 1 indi cates generally a tripod of either the M77 or M1917 tion between the frame and yoke.
ice
mount class and consisting of ground engaging legs 2 adjustably mounted to a pintle socket member 3. 4 indicates generally a cradle section, comprising a yoke member 5 pivotally mounted by a nut and a bolt 6 to a pintle frame section 7. Belleville spring washers 8, Figure 8, between the frame 7 and yoke 5 provides fric- Elevational control of the yoke 5 is obtained by turning a hand wheel 9 mounted at one end of an elongated shaft 10 journaled in bearings 11 integrally mounted from the lower surface of yoke 5. A worm 12 is fixed on the other end of shaft 10 and meshes with a pair of arcuate internal gear segments 13 fixed to the floor of the frame 7. Additional frictional braking action is afforded the yoke, necessary to overcome the unbalance of the launcher about the pivot 6 when elevating or depressing, by a brake member 14 carried by the forward under surface of 'the yoke 5 and which bears against the inner sides of the gear segments 13. A pintle 16 is attached to the under face of frame 7 by bolts 15 and is adapted to fit within the pintle socket member 3 of the tripod 1 whereby the frame and parts supported thereby may be trained as a unit in azimuth.-
Forward and rearward mounting lugs 17 and 18 are formed integrally on the respective ends of the upper surface of yoke member 5 for mounting forward and rearward launcher tube mounting bands 19 and 20 respectively, by pins 21 and 22. These bands are adapted to receive the launcher tube 23. The bands 19 and 20 are similar in construction and consist of afiexible strap adapted to surroundthe tube of the launcher.
As clearly shown upon Figure 5, each band is formed with an adjustable connection whereby its effective length may be varied to contract the same about the launcher tube. Thus, referring to Figures 5 and 6, one end of each strap is split and the two parts thus formed are rolled or looped as at 2311 to rotatably receive the ends of a draw pin 23b. The mid portion of this pin is transversely drilled to rotatably accommodate a screw 24a whose threaded end engages a tapped hole in the other and thickened end 24 of the strap. Thus each band may be contracted about the tube by turning of screw 24a.
From inspection of Figures 2 and 5 it will be noted that each strap has a tapered undercut lug or bracket 25 secured, as by welding, to its lower surface. Each lug forms a portion of a bayonet joint for a purpose subsequently explained. Similar tapered lugs 26 are provided upon the upper and outer side of the bands 19 and 20.
Spaced depending apertured ears or lugs 27 are provided on each of the bands 19 and 29 on respective sides of the lug 25 for mounting the bands on the yoke member 5. This mounting is effected by pins 21 and 22 which pass through the respective pairs of depending ears and the upstanding lugs 17 and 18 on yoke member 5, received between them. The lugs 25 and 26 are adapted to receive tapered clips 29 and 30 respectively, fixed to the ends of a shoulder stock 28. The shape and construction of this guard are obvious from inspection of Figures 1, 4 and 5. Figure 4 shows the guard attached to lugs 26 while Figures 1 and 5 show it attached to lugs 25.
To install the mounting bands 19 and 20 upon a launcher tube, bands 19 and 20 are placed about the tube and clamped thereto by turning the screws 24a. The bands are then attached to the cradle section by the pins 21 and 22, and the assembly is mounted to the tripod 1 by insertion of the pintle 16 into the pintle socket 3 of same. The shoulder stock 28 is mounted upon lugs 26 by its clips 29 and 30 whereby it is secured in the position shown upon Figure 4. The launcher is now in position for firing from prone or sitting position.
To prepare the launcher for shoulder firing, the mountin'g bands 19 and 20 are disengaged by' removing pins 21 and 22 and lifting the launcher from the cradle. The
shoulder stock is disengaged fromits position onlugs 26s the clip 30 to slide forward on its lug. Strike, the stock'- firmly with the hand to secure the clip (see Figure The launcher is now ready for use as a shoulder fire piece. It is to be noted that the natural resilience of the metal of stock 23 retains it against displacement'from the lugs 25. V g 7' Fromthe foregoing, it can beseen that a l'auncher mount has been provided that can be quicklyconverted from a ground mount to, a shoulder mount with a' minimum amount of manipulation. Greater mobility 'isalsoachieved as well as a lighter launcher due 'to elimination of the tripod when used as a shoulder firing piece. The mounting band may be of welded construction throughout to provide greater strength. The shoulder stock may be of lightweight construction and may be'ribbed for rigidity. p
It is to be understood that the form of the invention herein shown and described, is to be taken as a preferred example of the same, and that various changes in the shape, size and arrangements of parts may be resorted towithout departing from the spirit of my'invention, or the scope of the subjoined claims.
What is claimed is:
1. In a mount for a rocket launcher tube, a pair of split rings encircling said tube, in axially spaced relation therealong, each said ring terminating at one of their ends thereof in a pair of spaced loops and at their other ends in a thickened portion, means for tightening said rings about said tube comprising a draw pin rotatably'mounted in said loops, a screw transversely piercing said draw pins at a medial point and loops, each said screw to" be received" in a threaded hole being disposed between said in each said thickened portion, a tapered bracket secured to the underside of each said ring and a shoulder stock having a tapered clip secured to its respective ends adapted to'fit a respectiye hraeket on said rings, said brackets and said clipsltapering inopposite directions whereby theflresiliency of said stock. releasably' retains said stock on'a pair of said brackets;
2. In a mount fora/rocket launcher tubega pair of bands clamped abouLsaid tube in axially' spacefd relation therealong, a tapered mounting b'racket sepured to each said band, each said lug tapering-:iri' an opposite direction with respect to the othen a shoulder stock: comprising a I Refereed; Cited in the file this patent
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US570196A US2913960A (en) | 1956-03-07 | 1956-03-07 | Light weight t-20 shoulder stock for 3.5 inch rocket launcher |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US570196A US2913960A (en) | 1956-03-07 | 1956-03-07 | Light weight t-20 shoulder stock for 3.5 inch rocket launcher |
Publications (1)
Publication Number | Publication Date |
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US2913960A true US2913960A (en) | 1959-11-24 |
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ID=24278654
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US570196A Expired - Lifetime US2913960A (en) | 1956-03-07 | 1956-03-07 | Light weight t-20 shoulder stock for 3.5 inch rocket launcher |
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US (1) | US2913960A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1266665B (en) * | 1966-06-15 | 1968-04-18 | Boelkow Gmbh | Launching and steering device for recoil-propelled missiles starting from launch tubes with detachable visor carrier |
US3848508A (en) * | 1973-06-07 | 1974-11-19 | D Bullinger | Infantry attack vehicle with resilient armor |
EP0022431A2 (en) * | 1979-07-06 | 1981-01-14 | Förenade Fabriksverken | Shoulder support for fire arms |
FR2492083A1 (en) * | 1980-10-14 | 1982-04-16 | Serat | ANTICHAR ROCKET LAUNCHER |
FR2535449A1 (en) * | 1982-10-29 | 1984-05-04 | Thomson Brandt | Aiming device for a large-calibre personal fire arm |
US5854440A (en) * | 1995-10-30 | 1998-12-29 | The United States Of America As Represented By The Secretary Of The Navy | Shoulder-launched multi-purpose assault weapon |
FR2818369A1 (en) * | 2000-12-15 | 2002-06-21 | Realisations Et D Applications | Shoulder-held weapon for high-impulse munition such as mortar has non-consumable launcher and consumable container tube |
US6453594B1 (en) * | 1997-09-11 | 2002-09-24 | R/M Equipment, Inc. | Apparatus for attaching a supplemental device to a minimally altered host firearm |
US6598330B2 (en) * | 2000-09-14 | 2003-07-29 | Robert Hudson Garrett | Sling attachment hardware for firearms |
US6810614B2 (en) * | 2001-05-14 | 2004-11-02 | Alphonse E. Phillips | Devices, apparatuses and methods for mounting accessories to weapons including a scent generating device |
US20100051660A1 (en) * | 2008-09-04 | 2010-03-04 | Guy Noffsinger | Shoulder-mounted equipment carrier |
US20100287808A1 (en) * | 2009-05-16 | 2010-11-18 | Johnathan King | Loop-shaped Sling Adapter for use on Buffer Tube Assembly or Rifle Stock |
US8051596B1 (en) * | 2008-11-11 | 2011-11-08 | Thomas Jr James G | Hands-free firearm stabilizer |
US20160153743A1 (en) * | 2013-07-17 | 2016-06-02 | ROBERT Craing HAWKINS | An Accessory For A Firearm |
EP3112796A1 (en) * | 2015-07-01 | 2017-01-04 | Anortec, SL | Swiveling mount for a lightweight missile launcher having a single-use launch tube |
USD864335S1 (en) * | 2018-02-27 | 2019-10-22 | Cihan Sadik Yurek | Rocket projector |
Citations (12)
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---|---|---|---|---|
US1142602A (en) * | 1915-04-05 | 1915-06-08 | Alexander Miclaus Jr | Gun-mount. |
US1150763A (en) * | 1914-11-07 | 1915-08-17 | Frederick Herman High | Pistol-stock gun. |
US1315215A (en) * | 1919-04-14 | 1919-09-09 | Jacob Alexander Davidson | Rifle-stock. |
US1746364A (en) * | 1928-05-31 | 1930-02-11 | Rheinische Metallw & Maschf | Automatic firearm |
US1909171A (en) * | 1931-03-23 | 1933-05-16 | Richard C Coupland | Shoulder stock for machine guns |
US2333379A (en) * | 1941-04-26 | 1943-11-02 | Melvin M Johnson | Bayonet |
US2434162A (en) * | 1942-09-09 | 1948-01-06 | Bombs | |
US2466714A (en) * | 1948-04-26 | 1949-04-12 | William J Kroeger | Recoilless firearm and ammunition therefor |
US2472111A (en) * | 1945-02-14 | 1949-06-07 | William J Kroeger | Recoilless firearm and ammunition therefor |
US2537062A (en) * | 1949-02-02 | 1951-01-09 | William J Kroeger | Firing and safety mechanism for recoilless firearms |
US2742820A (en) * | 1952-12-15 | 1956-04-24 | Brown Robinson | Contact and stop mechanism for launchers |
US2779244A (en) * | 1954-07-29 | 1957-01-29 | Stephen A Stam | Lightweight cradle rocket launcher mount |
-
1956
- 1956-03-07 US US570196A patent/US2913960A/en not_active Expired - Lifetime
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1150763A (en) * | 1914-11-07 | 1915-08-17 | Frederick Herman High | Pistol-stock gun. |
US1142602A (en) * | 1915-04-05 | 1915-06-08 | Alexander Miclaus Jr | Gun-mount. |
US1315215A (en) * | 1919-04-14 | 1919-09-09 | Jacob Alexander Davidson | Rifle-stock. |
US1746364A (en) * | 1928-05-31 | 1930-02-11 | Rheinische Metallw & Maschf | Automatic firearm |
US1909171A (en) * | 1931-03-23 | 1933-05-16 | Richard C Coupland | Shoulder stock for machine guns |
US2333379A (en) * | 1941-04-26 | 1943-11-02 | Melvin M Johnson | Bayonet |
US2434162A (en) * | 1942-09-09 | 1948-01-06 | Bombs | |
US2472111A (en) * | 1945-02-14 | 1949-06-07 | William J Kroeger | Recoilless firearm and ammunition therefor |
US2466714A (en) * | 1948-04-26 | 1949-04-12 | William J Kroeger | Recoilless firearm and ammunition therefor |
US2537062A (en) * | 1949-02-02 | 1951-01-09 | William J Kroeger | Firing and safety mechanism for recoilless firearms |
US2742820A (en) * | 1952-12-15 | 1956-04-24 | Brown Robinson | Contact and stop mechanism for launchers |
US2779244A (en) * | 1954-07-29 | 1957-01-29 | Stephen A Stam | Lightweight cradle rocket launcher mount |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3389637A (en) * | 1966-06-15 | 1968-06-25 | Bolkow Gmbh | Firing and guiding mechanism for jetpropelled missiles launched from launcher tubes |
DE1266665B (en) * | 1966-06-15 | 1968-04-18 | Boelkow Gmbh | Launching and steering device for recoil-propelled missiles starting from launch tubes with detachable visor carrier |
US3848508A (en) * | 1973-06-07 | 1974-11-19 | D Bullinger | Infantry attack vehicle with resilient armor |
EP0022431A2 (en) * | 1979-07-06 | 1981-01-14 | Förenade Fabriksverken | Shoulder support for fire arms |
EP0022431A3 (en) * | 1979-07-06 | 1981-04-29 | Forenade Fabriksverken | Shoulder support for fire arms |
FR2492083A1 (en) * | 1980-10-14 | 1982-04-16 | Serat | ANTICHAR ROCKET LAUNCHER |
FR2535449A1 (en) * | 1982-10-29 | 1984-05-04 | Thomson Brandt | Aiming device for a large-calibre personal fire arm |
US5854440A (en) * | 1995-10-30 | 1998-12-29 | The United States Of America As Represented By The Secretary Of The Navy | Shoulder-launched multi-purpose assault weapon |
US6453594B1 (en) * | 1997-09-11 | 2002-09-24 | R/M Equipment, Inc. | Apparatus for attaching a supplemental device to a minimally altered host firearm |
US6598330B2 (en) * | 2000-09-14 | 2003-07-29 | Robert Hudson Garrett | Sling attachment hardware for firearms |
FR2818369A1 (en) * | 2000-12-15 | 2002-06-21 | Realisations Et D Applications | Shoulder-held weapon for high-impulse munition such as mortar has non-consumable launcher and consumable container tube |
US6810614B2 (en) * | 2001-05-14 | 2004-11-02 | Alphonse E. Phillips | Devices, apparatuses and methods for mounting accessories to weapons including a scent generating device |
US20100051660A1 (en) * | 2008-09-04 | 2010-03-04 | Guy Noffsinger | Shoulder-mounted equipment carrier |
US8051596B1 (en) * | 2008-11-11 | 2011-11-08 | Thomas Jr James G | Hands-free firearm stabilizer |
US20100287808A1 (en) * | 2009-05-16 | 2010-11-18 | Johnathan King | Loop-shaped Sling Adapter for use on Buffer Tube Assembly or Rifle Stock |
US20160153743A1 (en) * | 2013-07-17 | 2016-06-02 | ROBERT Craing HAWKINS | An Accessory For A Firearm |
EP3112796A1 (en) * | 2015-07-01 | 2017-01-04 | Anortec, SL | Swiveling mount for a lightweight missile launcher having a single-use launch tube |
USD864335S1 (en) * | 2018-02-27 | 2019-10-22 | Cihan Sadik Yurek | Rocket projector |
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