GB2555616A - Modular charge container - Google Patents

Modular charge container Download PDF

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Publication number
GB2555616A
GB2555616A GB1618622.3A GB201618622A GB2555616A GB 2555616 A GB2555616 A GB 2555616A GB 201618622 A GB201618622 A GB 201618622A GB 2555616 A GB2555616 A GB 2555616A
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United Kingdom
Prior art keywords
combustible
modular
canister
cartridge
energetic material
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.)
Granted
Application number
GB1618622.3A
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GB2555616B (en
Inventor
Marie Wilton Anne
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 GB1618622.3A priority Critical patent/GB2555616B/en
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Priority to EP17790819.1A priority patent/EP3535544B1/en
Priority to AU2017352845A priority patent/AU2017352845B2/en
Priority to US16/347,231 priority patent/US11125541B2/en
Priority to PCT/GB2017/053160 priority patent/WO2018083440A1/en
Publication of GB2555616A publication Critical patent/GB2555616A/en
Priority to IL266278A priority patent/IL266278B2/en
Priority to ZA2019/02764A priority patent/ZA201902764B/en
Application granted granted Critical
Publication of GB2555616B publication Critical patent/GB2555616B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/18Caseless ammunition; Cartridges having combustible cases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/38Separately-loaded propellant charges, e.g. cartridge bags
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/02Blasting cartridges, i.e. case and explosive adapted to be united into assemblies

Abstract

A modular charge container device is formed of one or more combustible modular cartridges 40. Each combustible modular cartridge 40 comprises two ends, a first end comprising a base portion and a second end comprising a top portion. The combustible modular cartridge 40 is formed using a substantially rigid and combustible material and comprises at least one wall 41 to define a cavity. The cavity further comprises at least one combustible canister 43 which comprises an energetic material.

Description

(54) Title of the Invention: Modular charge container Abstract Title: Modular charge container device (57) A modular charge container device is formed of one or more combustible modular cartridges 40. Each combustible modular cartridge 40 comprises two ends, a first end comprising a base portion and a second end comprising a top portion. The combustible modular cartridge 40 is formed using a substantially rigid and combustible material and comprises at least one wall 41 to define a cavity. The cavity further comprises at least one combustible canister 43 which comprises an energetic material.
Figure GB2555616A_D0001
At least one drawing originally filed was informal and the print reproduced here is taken from a later filed formal copy.
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Fig.1 (Prior Art)
Figure GB2555616A_D0002
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Fig. 2 (Prior Art)
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Figure GB2555616A_D0003
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Fig. 3a
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Figure GB2555616A_D0004
Fig. 3b
Figure GB2555616A_D0005
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Fig. 3c
Figure GB2555616A_D0006
Figure GB2555616A_D0007
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Figure GB2555616A_D0008
Figure GB2555616A_D0009
Fig. 5a
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Figure GB2555616A_D0010
Fig. 5b
Figure GB2555616A_D0011
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01 18
Fig. 6
Figure GB2555616A_D0012
- 1 Modular Charge Container
The invention relates to a charge container, for use as a charge for propelling munitions, more specifically related to the area of modular charge containers.
Within the field of munitions a projectiles range may be achieved by utilising an explosive train sequence, which may comprise an igniter, a primer with an intermediate explosive and an output charge. The explosive train serves to take a small energetic event and amplify the output as it moves through the explosive train.
In military use, an explosive train sequence is often used in the launching of munitions, whether direct or indirect; to propel a shell over a distance, often considering a minimum launch distance to prevent injury to own troops or large distances to reach long range. To accomplish an explosive train sequence relating to a specific distance, an ignition means is incorporated alongside a charge, with additional charges being added or subtracted depending on the distance the shell is to travel.
The construction of an explosive train sequence may be carried out modularly; this can be done in a number of ways depending on the system used and various other user requirements or conditions (e.g. variations of distances where opposition forces are engaged).
One example of the use of a combination of charges to achieve a launch distance is to load modular charges individually into the breach until the desired total charge is achieved. Each charge contains an energetic material and is made from a rigid, combustible case and may be of different sizes, which correspond to a predetermined distance they are able to propel a shell. Each charge comprises a recessed and extruded portion to allow them to fit together as they are loaded into the breach in order to prevent adverse movement. In use the ignition means on the case (e.g. an igniter pad) is struck and causes an explosive train sequence to begin, which continues through the charges until the force expels the shell from the barrel of the weapon.
-2This method suffers as the explosives train is formed by utilising the individual charges loosely coupled together utilising the recess/extrusions provided, making rapid movement or formation of a desired charge time consuming. The charges themselves are also formed from a rigid outer case containing loose energetic material and as a result hold no flexibility for rapid change of energetic material quantity if needed.
Another example is utilising a chain of combustible bags, combustible in this context refers to the fact that the bags are fully consumed following burning, rather than providing further energetic output. These combustible bags are filled with a set quantity of energetic material, relating to different distances the shell is to be launched. These bags may be placed into a single, larger combustible bag (e.g. cotton), with an igniter pad at the base wherein the total number of bags contained within relate to a specific distance. Alternatively the number of required bags is placed in an initial combustible bag, which comprises a number of ties that may be brought up around the combustible bags to hold them in place. When required to be used the larger bag or combustible bag chain is taken and placed in its entirety into the breach. Upon firing the ignition begins the explosive train, which travels up through the bags, firing the shell over the desired distance and combusting the bag in the process, allowing the breach to be clear for the next shell and charge.
This method has significant cost savings and flexibility as the use of a large single bag to contain smaller charges means that a single bag, relating to a distance can be moved around and is not costly to produce. Its lack of rigid structure does however make handling difficult and a cotton material can be prone to snagging and tears. Further to this the adding of single bags to a larger container can be subject to human error and mistakes, such as the addition of the wrong charge or omission of a charge, may cause a launch to overshoot or undershoot its target. These human errors may increase during periods of high stress, such as conflict.
A final example involves a single full length master combustible bag with individual “elongate sticks” of energetic material contained in individual full length combustible bags. There is a selection of different combustible bags
-3which are filled with different specific amounts of propellant. The sticks, once in their combustible bags are arranged to run the full length of the single master combustible bag. In use an ignition pad at the bottom of the single master combustible bag is struck and causes the “elongate sticks” of energetic material to react and burn from the base of the master bag up through the “elongate stick”.
This method has the advantage that it is easier to add or remove the combustible bags of energetic material to the single master combustible bag. As a result the distance a shell is to travel may be adjusted as required. Like other methods however this method is prone to human error resulting in the incorrect arrangement of combustible bags or damage to the combustible bags during handling.
The invention herein aims to address the issues presented in the background prior art by solving issues in robustness, flexibility and usability.
According to a first aspect of this invention there is provided a modular charge container device formed of one or more combustible modular cartridges, wherein said combustible modular cartridge comprises two ends, a first end comprising a base portion and a second end comprising a top portion, wherein the combustible modular cartridge is formed using a substantially rigid and combustible material, said combustible modular cartridge comprises at least one wall to define a cavity, wherein the cavity further comprises at least one combustible canister, wherein said combustible canister comprises an energetic material.
The said modular combustible cartridge may be produced as a single unit, preferably each modular cartridge is of fixed length and diameter, such that the dimensions are determined depending on the breach it is designed to fit and the amount and type of energetic material the combustible cartridge is intended to hold.
-4A plurality of modular combustible cartridges may be stacked one on top the other, to produce a modular charge container device, for use in a breach to project the round or shell.
The combustible cartridge is constructed from a rigid and combustible material, such as a cardboard impregnated with an energetic substance for example, which allows the combustible cartridge to be moved easily. The combustible cartridge will combust to leave substantially no residue after the firing event to prevent the need to clean the barrel or remove debris prior to loading a new shell, combustible modular cartridges or charge container.
In one arrangement of the combustible modular cartridge’s base portion comprises a base cover with an aperture therein, wherein said base cover may comprise a recessed portion to allow the insertion of a protrusion on the surface of a top portion of a further combustible modular cartridge. This will allow further combustible modular cartridges to be added or removed to create the desired final length of modular charge container, so as to form the required effect of the explosive train as necessary, depending on the distance that the shell is to travel. The addition or removal of combustible modular cartridges may be achieved by the insertion or removal of the top portion of one of the combustible modular cartridges into another as they are formed to be placed into the breach.
In a further arrangement the base cover and top cover may comprise mating surfaces to provide cooperative engagement between said top cover and base cover.
The mating surfaces may be provided by co-operatively engaged protrusion and recessed portions, and may be swapped in design to allow a protrusion on the base of the combustible modular cartridge to be slotted into a recess on the top portion of the combustible modular cartridge.
In a further arrangement both top portion and base portion may comprise an abrasive surface or a surface with raised portions to increase the coefficiency of friction of the two surfaces in order that when a top portion and a base portion are in contact they are sufficiently resilient to movement.
In an further arrangement subsequent combustible modular cartridges may be joined to adjacent combustible modular cartridges by a releasable
-5means, or reversible locking engagement means, such as, for example a hook and loop arrangement (e.g. Velcro) or a press and lock arrangement. A yet further example may be provided by utilising a hook on either the top portion or base portion that would engage with a recessed bar on the top portion or base portion of a connecting combustible modular cartridge.
The combustible modular cartridge’ wall defines a cavity, which houses a combustible canister therein. The combustible canister contains a set amount of energetic material; said amount of energetic material may be dependent on the distance required of the propelled munition (e.g. a shell). This amount will relate directly to a designation on the combustible modular cartridge to allow selection for use in an explosive train.
In a preferred arrangement each combustible canister has a uniform mass of propellant such that a set number of increments may be selected.
The combustible container may be formed from a rigid material similar to that of the cartridge case (e.g. cardboard), however in a preferred embodiment will be a flexible material such as cotton, as it is cheaper and faster to manufacture as well as providing a simpler system to add the energetic material. This provides a further advantage, allowing a flexibility to manage energetic material quantity, preventing over-ordering and potential wastage.
The combustible canister may be housed in the cavity, preferably utilising a releasable attaching means to the wall of the combustible modular cartridge. The releasable means may comprise a hook and loop releasable attachment (e.g. Velcro).
In a further arrangement the combustible container may be held in place by one or more spacers attached to the wall of the combustible modular cartridge. The spacers may hold each added combustible canister in place, providing a gap allowing for the propagation of a flame front in the gap between the combustible canister and the combustible modular cartridge. The gap may be greater than 1mm and preferably in the range of from 1mm to 30mm, more preferably 1mm to 10mm. The use of spacers provides a more uniform burn as the flame front can propagate in the gap, and hence a more uniform explosive
-6energy output from the combustible modular cartridge may be achieved. The gap may provide a path for both thermal output and flame propagation, allowing the device to utilise the areas created by the spacers to ensure even ignition of the combustible modular cartridge and energetic material within the combustible canister.
The combustible canister comprises at least one energetic material, which may be a material such as a pyrotechnic, propellant or high explosive composition.
The addition of energetic material to a combustible canister either within the cartridge or prior to addition to the cartridge has a number of advantages. It allows the amount of energetic material within a cartridge to be adapted as required, without the need to manage the energetic material directly, which may lead to incorrect amounts of energetic material being added and allows a single cartridge size to have differing effects as needed. It also allows the indirect management of the energetic material spacing as the combustible canister may be manipulated into position to provide a gap for the flame front (for example) or wrapped around (or space provided for) a central igniter.
The base portion of the combustible modular cartridge may comprise an igniter pad, said igniter pad being present to aid in the initiation of the explosive train and in a preferred arrangement will contain an energetic material such as a propellant or pyrotechnic.
In an alternative arrangement ignition is achieved utilising a central igniter, comprising a propellant or pyrotechnic and running from the base portion to the top portion of the combustible modular cartridge. This central igniter allows an even ignition to the energetic material within the combustible canister.
Whilst the invention has been described above, it extends to any inventive combination of the features set out above, or in the following description, drawings or claims.
-7Exemplary embodiments of the device in accordance with the invention will now be described with reference to the accompanying drawings in which:Figure 1 shows a schematic view of a prior-art cartridge with energetic material contained within.
Figures 2 shows the design currently in use.
Figures 3a, 3b, 3c and 3d show a number of views of the combustible modular cartridge with 3a showing a plurality of combustible modular cartridges arranged cooperatively attached, 3b shows a cross-section of 3a, 3c shows a top-down view of a single combustible modular cartridge and 3d shows a bottom up view of a single combustible modular cartridge.
Figure 4a and 4b show a cross section of an embodiment of the combustible modular cartridge with differing cooperative attachment means.
Figure 5a and 5b show a top-down view of the combustible modular cartridge in alternative arrangements.
Figure 6 shows a schematic of a plurality of coaxially aligned combustible modular cartridges, arranged in a stacked arrangement.
Referring to Fig 1, there shows a prior art arrangement wherein energetic material 13 is loosely contained within a charge 10, shaped to be co-operably engaged with charges of the same type. In this prior art embodiment, no separate container of energetic material is used. As a result energetic material 13 is left loose within the charge 10, preventing any ability to accurately adapt or modify the charge yield if required. Further to this no management of the explosive train is presented by the use of a gap between the energetic material and the wall of the charge.
Fig 2 shows a further prior art arrangement which comprises individual combustible bags 28 being placed in a stacked arrangement to form the output charge 29. The combustible bags 28 may be held in place to prevent movement by a base 25 and strips of combustible material 22, which are tied in a knot to hold the combustible bags in the stacked arrangement. This method provides little to no stability during movement of the plurality of combustible bags 28.
-8Fig 3a and 3b show a stacked arrangement according to the invention. There is a plurality of combustible modular cartridges 20, wherein each combustible modular cartridge is cooperatively engaged with a further combustible modular cartridge 20, which may be located either above or below. The combustible modular cartridges 20 comprise a combustible canister 23, located therein. The combustible canister 23 comprises an energetic material, such as a grain or stick propellant. The combustible canister 23 may be reversibly attached to the combustible modular cartridge at least one wall 21 by a reversible means 24, in order to form a gap 27. The shape and rigidity of the combustible modular cartridge 20 allows for ease of movement, stability of storage and an ability to increase or decrease the number of combustible modular cartridges 20 depending on the output required.
Referring to Fig 3c, there shows a combustible modular cartridge top 20a comprising a combustible modular cartridge at least one wall 31, a combustible canister 33 located in the cavity, said combustible canister 33 comprising energetic material 32 and a plurality of spacers 37. The spacers 37 provide a gap 34 between the at least one wall 31 and the combustible canister 33. The combustible canister 33 and combustible modular cartridge 30 may be linked by a reversible attaching means. Fig 3d shows a combustible modular cartridge base 20b with an igniter pad 35 which is in thermal contact with the combustible canister (not shown). In use a force is exerted on the igniter pad 35 causing an ignition, which is transferred to the propellant in the combustible canister. The energetic material inside the combustible canister 33 comprises an energetic material which undergoes an exothermic reaction causing a release of heat and gas. The concomitant flame front thus formed, travels in the gap 34 formed between the combustible canister 33 and the combustible modular cartridge wall 31.
Referring to Fig 4a and 4b there is a cross sectional view of a combustible modular cartridge 40 with a combustible modular cartridge wall 41,
-9an internal combustible canister 43 comprising energetic material and a reversible attachment means 44 between said combustible modular cartridge wall 41 and combustible canister 43. Fig 4a and 4b both have protruding portions 46a and 46b and co-operative recessed portions 47a and 47b to enable cooperative engagement with successive combustible modular cartridges 40. This engagement may be a reversible means to enable a stronger link or a means of friction to prevent the combustible modular cartridge 40 from sliding apart. Fig 4a and 4b are examples, which show an arrangement where the protrusion portions 46a/b slides into the recessed portions 47a/b to enable controlled management of the combustible modular cartridge 40. This cooperative engagement may be independent of or including a charge container.
Referring to Fig 5a and 5b there is presented two potential arrangements of the top portion of the combustible modular cartridge. Fig 5a is arranged with a substantial aperture 58 to aid in the propagation of a produced flame front, the combustible canister 56 can be seen internal to the combustible modular cartridge, with spacers 57 being achieved utilising a hook and loop system e.g. Velcro. These may be used to secure the combustible canister 56 to the combustible modular cartridge, while providing a gap 54 for the flame front to travel in.
Fig 5b shows the top portion, with a recessed portion 55 to aid cooperative engagement with a further combustible modular cartridge with a cooperative raised portion (not shown) and a plurality of apertures 58 to aid in the propagation of a produced flame front.
Referring to Fig 6 there is presented a cross-sectional view of a modular charge container 67, arranged by utilising a plurality of combustible modular cartridges 60. The modular charge container 67 is arranged in a stacked, coaxial arrangement, utilising a cooperative engagement means as identified in fig 4a. The base portion of the modular charge container 67 comprises an igniter pad 63 fitted to the combustible modular cartridge. In use the igniter pad
-IQ63 is struck, beginning the explosive chain through the combustible modular cartridges 60.

Claims (15)

Claims:
1) A modular charge container device formed of one or more combustible modular cartridges, wherein said combustible modular cartridge comprises two ends, a first end comprising a base portion and a second end comprising a top portion, wherein the combustible modular cartridge is formed using a substantially rigid and combustible material, said combustible modular cartridge comprises at least one wall to define a cavity, wherein the cavity further comprises at least one combustible canister, wherein said combustible canister comprises an energetic material.
2) A device according to claim 1, wherein there is a gap between the at least one wall and the combustible canister, such as to allow the propagation of a flame front
3) A device according to claim 2, wherein the gap is in the range of from 1mm - 10mm.
4) A device according to claims 2 to 3, wherein at least one spacer is located in the gap between the at least one wall and the combustible canister.
5) A device according to any preceding claim, wherein the combustible canister is reversibly attached to the at least one wall.
6) A device according to any preceding claim wherein the base portion comprises a base cover with an aperture therein.
7) A device according to any preceding claim wherein the top portion comprises a top cover with an aperture therein.
-12
8) A device according to claim 7, wherein said base cover and top cover comprises mating surfaces to provide cooperative engagement between said top cover and base cover.
9) A device according to claim 8 wherein the top cover and base cover mating surfaces comprise a high co-efficient of friction, or at least one raised or recessed portion to retain engaged combustible modular cartridges.
10) A device according to any preceding claim, wherein the top portion and base portion may be reversibly locked together.
11) A device according to claim 10, wherein the top portion and base portion may be reversibly locked together by the use of a recessed bar and hook arrangement or twist lock arrangement.
12) A device according to any preceding claim wherein the one or more combustible modular cartridges are the same dimensions and comprise the same mass of energetic material.
13) A device according to any preceding claim, wherein the combustible canister is constructed from a flexible material.
14) A device according to any preceding claim, wherein the flexible material is cotton cloth or polyester cloth.
15) A device according to any preceding claim, wherein the device comprises a central igniter running from the base portion to the top portion.
-1316) A method of forming a modular charge container as described in anyone of claims 1-15, comprising the steps of filling a combustible canister with an energetic material, locating said combustible canister inside the combustible modular cartridge.
Intellectual
Property
Office
Application No: GB1618622.3 Examiner: Peter Macey
GB1618622.3A 2016-11-04 2016-11-04 Modular charge container Active GB2555616B (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB1618622.3A GB2555616B (en) 2016-11-04 2016-11-04 Modular charge container
AU2017352845A AU2017352845B2 (en) 2016-11-04 2017-10-19 Modular charge container
US16/347,231 US11125541B2 (en) 2016-11-04 2017-10-19 Modular charge container
PCT/GB2017/053160 WO2018083440A1 (en) 2016-11-04 2017-10-19 Modular charge container
EP17790819.1A EP3535544B1 (en) 2016-11-04 2017-10-19 Modular charge container
IL266278A IL266278B2 (en) 2016-11-04 2019-04-28 Modular charge container
ZA2019/02764A ZA201902764B (en) 2016-11-04 2019-05-02 Modular charge container

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1618622.3A GB2555616B (en) 2016-11-04 2016-11-04 Modular charge container

Publications (2)

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GB2555616A true GB2555616A (en) 2018-05-09
GB2555616B GB2555616B (en) 2021-10-06

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GB1618622.3A Active GB2555616B (en) 2016-11-04 2016-11-04 Modular charge container

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US (1) US11125541B2 (en)
EP (1) EP3535544B1 (en)
AU (1) AU2017352845B2 (en)
GB (1) GB2555616B (en)
IL (1) IL266278B2 (en)
WO (1) WO2018083440A1 (en)
ZA (1) ZA201902764B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2555618B (en) 2016-11-04 2021-12-29 Bae Systems Plc Munition charge container
GB2555616B (en) 2016-11-04 2021-10-06 Bae Systems Plc Modular charge container

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Also Published As

Publication number Publication date
EP3535544B1 (en) 2021-06-23
US11125541B2 (en) 2021-09-21
EP3535544A1 (en) 2019-09-11
IL266278B (en) 2022-10-01
US20190277606A1 (en) 2019-09-12
ZA201902764B (en) 2021-09-29
IL266278A (en) 2019-06-30
GB2555616B (en) 2021-10-06
AU2017352845A1 (en) 2019-05-23
WO2018083440A1 (en) 2018-05-11
AU2017352845B2 (en) 2023-02-02
IL266278B2 (en) 2023-02-01

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