OBSCURANT DEVICE

Abstract: Many of today's weapons systems use surveillance and target acquisition (STA) devices which can exploit the infrared and millimetre wavebands of the electromagnetic spectrum. Designing obscurant devices which can provide screening against such systems often results in complicated or costly solutions. A device capable of mitigating these problems is described wherein an obscurant device (10), and more particularly a device capable of providing screening against the visual, infrared and millimetre wave regions of the electromagnetic spectrum, comprises an obscurant payload, a burster charge capable, when detonated by a detonator, of disseminating said payload and a payload casing wherein some or all of the payload casing is configured to disintegrate upon actuation of the burster charge and to act thereafter as an obscurant.

Description: OBSCURANT DEVICE The present invention relates to obscurant devices and more particularly to those capable of providing screening against the visual, infrared and millimetre wave regions of the electromagnetic spectrum. It has long been a desire to increase the survivability of friendly forces m battle by screening them from enemy sensors. Historically, smoke has been used to achieve this aim. However, advances m the field of sensor technology has increased the effectiveness of many weapons systems by equipping them w th surveillance and target acquisition (STA) devices which can exploit the infrared and millimetre wavebands of the electromagnetic spectrum. Longer wavelength radiation is readily transmitted through conventional visual obscurant screens thereby exposing friendly forces to greater risks. Research has shown that there is currently no single material that is capable of screening effectively at visual, infrared and millimetre wavelengths. Since obscurant materials screen radiation whose wavelength is roughly equal to their particle size it is highly improbable that a single material capable of screening across the millimetre to infrared range will be developed m the near future. In order, therefore, to provide protection against STA devices it is necessary to deploy a mixture of obscurants, for example powders, fibres and pyrotechnic compositions, from a single munition. There is currently no "commercial off the shelf" device which comprises a mixture of components designed to counter STA devices However, a design for such a device was disclosed m the Smoke/Obscurants Symposium, 28-30 April 1998, Aberdeen Proving Ground, Maryland, USA, The Evolution of a Design for a Rapid Bloom Mul ti -Spectral Obscurant Muni tion by P J D Collins, J M B Chπstofi, N Davies and D Green A disadvantage of this design is that it would tend to be relatively large and complex and therefore expensive to manufacture A further disadvantage of this device is that the munition has a section with a calibre that is larger than the standard US and UK calibre. The only known millimetre wave screening munition is the United States M81 66 millimetre grenade (NATO Classification; Grenade Launcher Smoke: MM/IR screening M81) . A disadvantage of this grenade is that, although the design is capable of carrying some infrared screening payload, it is optimised for performance in the millimetre waveband. In practice, in order to achieve multi- spectral screening the US require the use of a number of different obscurant devices, e.g. one for infrared screening, one for visual screening and one (the M81) for millimetre screening. It is therefore an object of the present invention to provide an obscurant device which alleviates some of the above disadvantages by constructing part or all of the device payload casing from a material that contributes to the screening effect of the device. Accordingly, the present invention provides an obscurant device comprising an obscurant payload, a detonator, a burster charge which is initiated by action of the detonator and which is capable of disseminating said payload and a payload casing wherein some or all of the payload casing is configured to disintegrate upon actuation of the burster charge and to act thereafter as an obscurant . Usefully the payload casing can be configured to provide effective electromagnetic screening in the millimetre waveband by constructing the casing out of a conductive carbon fibre. In this context effective millimetre wave attenuation is taken to be > lOdB (< 10% transmission) for a single pass through an obscurant cloud. Suitable fibre types for construction of the casing include : - i) UTS carbon fibre, a PAN (poly-acrylo-nitrile) based carbon fibre which has a Young's Modulus (YM) of 230 Gpa; II ) Nickel coated carbon (Ni-C) , a PAN based carbon fibre with a YM similar to UTS; III) UD cloth carbon (UD-C) , a unidirectional non-crimp material using carbon w th a YM = 230 Gpa; IV) J-UTS carbon fibre, similar to the UTS fibre above but with a higher strain to failure; v) PlOOs carbon fibre, a pitch based carbon fibre with higher electrical conductivity than that observed for PAN-based fibres; vi ) Ultra-high Modulus (UMS) carbon fibre, a high modulus PAN- based carbon fibre. It was found m tests that highest mean attenuation m the measured millimetre wavelengths was achieved when the casing was made from UMS carbon fibre. In order to achieve attenuation at the required frequencies the conductive casing should disintegrate into fibre lengths in the range of 1 mm to 10 mm. This is because the level of attenuation is maximised when the fibre-length is approximately a half- wavelength. For example, at 94 GHz (≡ 3mm) a fibre length of 1.5 mm is required. Furthermore, manufacture of the payload casing can conveniently be achieved by dry filament winding as described more fully hereinafter. The Applicant has found that manufacture of the payload casing by the above technique using commercially available carbon fibre naturally results m a structure that disintegrates upon detonation into individual fibres suitable for millimetre screening. Suitable carbon fibre can be obtained from, for example, the following companies. Tenax Plastics Limited, Akzo, Amoco, Courtaulds and Roskill. Conveniently, the device can carry a mixture of obscurants as payload m order to result m screening at multiple wavebands. For example, if the device carries a brass flake/red phosphorous payload then, m addition to the millimetre screening effect generated by the disintegrating payload casing, the device also screens in the infrared and visual wavebands A device as described above can conveniently be adapted for use as a munition or as a decoy flare for deployment from an aircraft or a ship. At present aircraft and ships use different infra-red and radar decoys. For use in aircraft the device described above would be loaded w th a magnesium/teflon/viton (MTV) payload and for naval uses a payload of red phosphorous would be appropriate. An embodiment of the present invention will now be described, by way of example, with reference to the accompanying drawings, wherein Figure 1 shows a cross-section of a device design according to the invention Figure 2 shows attenuation against time plot for the attenuation of the K Band (35 GHz) radiation for trial 1 (wind speed conditions < 2 ms 1 ) . Figure 3 shows attenuation against time plot for the attenuation of the M Band (94 GHZ) radiation for trial 1 Figure 4 shows the same attenuation versus time plot as figure 2 but for trial 2 (wind speed conditions between 7 ms 1 and 9 ms x ) Figure 5 shows the same waveband versus time plot as figure 3 but for trial 2 Figures 6 and 7 show the transmission against time at 5 specific wavelengths m the visual and infra red wavebands for trials 1 and 2 respectively Referring now to Figure 1 This figure shows a cross section through a typical multi -spectral obscurant device 10 In this embodiment the payload, brass flake 20, is contained within a spool 30 sealed with end caps 31, 32 The end caps 31, 32 have apertures through which tube 33 is fitted along the axis of the spool 30. Tube 33 is sealed to the end caps 31, 32 and to the spool 30 and contains high explosive pellets 40 comprising > 95% RDX (Hexahydro-1, 3 , 5-tπnιtro-l, 3 , 5-trιazme) , such as Debπx High Explosive pellets as manufactured by Royal Ordnance. A detonator 60 is located at one end of tube 33 and is connected to a fuze or firing box (not shown) by leads 61. The conductive UMS carbon fibre case 50 surrounds the spool and is added by dry filament winding (The process of dry filament winding involves winding the fibre off a reel, at a set fibre tension. The fibre is then passed through a winding eye and is finally wound onto a bobbin, i.e. m this case the spool) . During construction of the payload the fibre is initially wound onto itself a number of times m order to anchor itself to the spool. A pre-programmed winding program is then run until the desired mass is deposited onto the spool. The free end of the fibre is then bonded to the deposited fibre by using an adhesive. Alternatively the carbon fibre case 50 could be constructed separately. The components of the obscurant device 10 could then be assembled and the payload loaded into the device. In operation, an electric pulse from a fuze or firing box initiates the detonator 60. The exploding detonator 60 produces a shock wave which detonates the high explosive pellets 40. The detonation of the high explosive pellets 40 disseminates the payload, brass flake 20, and also causes the carbon fibre case 50 to disintegrate and to act thereafter as a millimetre waveband obscurant . During trials carried out on the obscurant device over 55 devices were tested. In all cases the conductive fibre casing had a diameter of 66 millimetres and was 160 millimetres m length. The particular carbon fibre used had a diameter of 7 microns . On average the total weight of the device with the carbon fibre casing was 1157 grams (this value varied from around 1100 to 1200 grams across the tested devices) . The average weight of carbon fibre casing was 159 grams (this value varied between 99 and 183 grams) . Twelve Debπx pellets were used as the burster charge. Figures 2 to 7 represent results which are typical of all the tested devices and as can be seen from figures 2 to 5 the carbon fibre casing generates an efficient obscurant field m the millimetre wavebands. Turning to figure 2 it can be seen that significant attenuation of the K band is achieved almost immediately following device detonation. Over 20 dB attenuation is recorded for the first ten seconds. Th s drops to around 8 dB for a few seconds before returning to 20 dB for another f ve seconds. Figure 3 shows that a screen of over 40 dB was initially formed m the M band and that this screen reduced to around 15 dB after eight seconds. It is therefore clear that significant attenuation within the millimetre waveband is achieved under low wind speed conditions by using the invention. Turning to figures 4 and 5 t can be seen that even under higher wind speed conditions an obscurant cloud capable of attenuating along the line of sight is generated. Effectiveness of the generated visual/mfrared obscurant cloud is not compromised by using the casing to generate the millimetre obscurant field. This can be ascertained by examination of the visual and infrared transmission data as detailed m figures 6 and 7. It can be seen that transmission at each of the five wavelengths monitored s immediately reduced to low levels once the device detonates. Effective obscuration varies from 8 to 30 seconds depending on the wind conditions d e high wind to low wind speed) . Further embodiments of the invention can be envisaged wherein different obscurant materials are used as the payload, i.e. red phosphorous or magnesium/teflon/viton (MTV) .

Claims: CLAIMS 1. An obscurant device comprising an obscurant payload, a detonator, a burster charge which is initiated by action of the detonator and which is capable of disseminating said payload and a payload casing wherein some or all of the payload casing is configured to disintegrate upon actuation of the burster charge and to act thereafter as an obscurant. 2. An obscurant device as claimed m claim 1 characterised in that some or all of the payload casing disintegrates upon detonation to form a millimetre waveband obscurant. 3. An obscurant device as claimed in claim 2 characterised in that the payload casing is made of a conductive carbon fibre. 4. An obscurant device as claimed in claim 3 characterised in that the conductive fibre is selected from UTS, Ni-C, UD-C, J-UTS, PlOOs and Ultra-high modulus carbon fibre. 5. An obscurant device as claimed n claim 4 characterised in that the payload casing is made of Ultra-high modulus carbon fibre . 6. An obscurant device as claimed in claims 2, 3 or 4 characterised in that the payload casing disintegrates upon detonation into fibre lengths of between 1 mm and 10 mm. 7. An obscurant device as claimed m claims 3, 4, 5 or 6 characterised m that the payload casing is constructed by carbon fibre winding. 8. An obscurant device as claimed m claims 3 to 7 characterised in that the carbon fibre has a diameter of 7 microns . 9. An obscurant device as claimed m any of the preceding claims characterised m that the obscurant payload is capable of providing obscuration at visual wavelengths. 10. An obscurant device as claimed in claim 9 characterised in that the obscurant payload comprises red phosphorous. 11. An obscurant device as claimed in any of the preceding claims characterised in that the obscurant payload is capable of providing obscuration at infrared wavelengths. 12. An obscurant device as claimed in claim 11 characterised in that the obscurant payload includes brass flakes. 13. A screening decoy flare suitable for deployment from an aircraft comprising an obscurant device as claimed in claims 1 to 11 carrying a payload of magnesium/teflon/viton. 14. An obscurant device as hereinbefore described with reference to the accompanying drawings .

Inventors: COLLINS PETER JOHN DAVID, COLLINS, PETER, JOHN, DAVID
Applicants: COLLINS PETER JOHN DAVID, SECR DEFENCE, COLLINS, PETER, JOHN, DAVID, THE SECRETARY OF STATE FOR DEFENCE
Application year: 2000
Main classification: F42B12
IPC codes: F42B5, F42B12