In the field of gun launched munitions, a need exists to provide accurate and consistent muzzle velocity of the munition, such as a gun launched projectile. This is done by providing a ‘shot start’ which may be a tab connected to the munition, and where the shot start tab juts out from the munition's exterior and is lodged in a mating cavity within the side of the launch tube. In order to launch the munition, there must be sufficient launch pressure on the munition to physically break the shot start. It can be seen that providing a shot start would be a means to provide a consistent launch velocity of these munitions as designed in such launch tubes. The munitions may embrace many types, such as shoulder fired weapons, multi target weapons, MOUT or other types. The munition may also be surrounded inside the gun tube by a sabot, or sabot comprised of multiple sections. It would be a further advantage to such munition launching systems if the shot start means and the sabot means were designed to be of one unitary piece. There would be advantages for weight, economics of manufacturing, construction and consistency of the structure.
An integrated sabot shot start projectile has been produced in accordance with this invention. The projectile sabots with an integrated shot start were parts developed on a MOUT (Military Operations in Urban Terrain) ATO SFW (Advanced Technology Objective Shoulder Fired Weapon) IAM requirement program. This program was to develop a shoulder fired weapon that would be lighter than current shoulder fired weapons but which could be used against multiple target sets. It is known that the chamber pressure of a gun directly affects the velocity of its projectile. So, in this gun launched system it was crucial to find a method to obtain an accurate and consistent gun chamber pressure to maintain an accurate and consistent muzzle velocity. Methods for obtaining the above mentioned consistent chamber pressure included providing a shot start tab. To meet the requirements of low weight and high velocity this system also utilized sabot technology. The system was accomplished by integrating the shot start tab onto the sabot of the projectile, as a unitary component of tab with sabot. The shot start was integrated on to the sabot for reasons including ease of assembly, positive visibility since it was seated in the gun groove, no interference with gun exit sabot discard, to help better seal the gun gases, and for lowering overall manufacturing costs. The sabot with an integrated shot start was developed to fit in sections around the body of the projectile and in this case the sabot had three 120 degree sections. A shear tab on the sabot would not only hold the projectile in place until broken at a predetermined pressure, but would also be used to correctly locate and lock the projectile into place. The tab on the sabot would line up with a corresponding tab or groove location in the gun tube. The sabot could have either a tab or a groove depending on the mating component of the gun tube. There are various ways of loading this type of munition (including shot start and sabot) into the launch tube. Methods include a split breach. Another method would include inserting the projectile through the aft end of the gun tube and rotating it into place when it reached the corresponding tab or groove location in the gun tube. At this point, the projectile could no longer move through the gun tube unless the shear tab on the sabot were broken. After the desired chamber pressure would be reached, the shear tab would fail at the shear groove and the projectile would be free to move down the gun tube. (This pressure is pre-determined based on the depth of the shear groove dimension in the tab and can be adjusted depending on firing requirements). The projectile then moves and follows typical interior ballistic patterns. The shot start portion of the sabot may be left over partially disposed of in the groove of the gun tube. Upon exit from the gun tube, the sabots discard without impedance from the body of the projectile. This invention served two purposes, (1) to load and hold the projectile in place inside the gun tube up to a certain pre-determined pressure and (2) to add sabots to the projectile to allow for maximum acceleration and muzzle velocity of the projectile until it is out of the gun tube. Although sabots have been used on other projectiles, this is the first attempt to integrate the sabots with a shot start feature. A radial shear groove on the tab allows the ring to fail at a determined pressure. During testing, the sabot sections with the integrated shot start ring worked as designed, and held the projectile in place until the desired chamber pressure was reached. After the chamber pressure was reached, the projectile traveled out the muzzle of the gun tube achieving the desired velocity. The sabot sections discarded off the body of the projectile during the first 5-10 meters after exit, without impeding the flight trajectory. The sabots were successful in all tested shots.
Accordingly, it is an object of the present invention to develop a shoulder fired weapon that would be lighter than current shoulder fired weapons but which could be used against multiple target sets.
Another object of the present invention is to develop a shoulder fired weapon with an accurate and consistent gun chamber pressure to maintain an accurate and consistent muzzle velocity.
It is a further object of the present invention to develop a shoulder fired weapon that will hold its projectile in place until a desired chamber pressure is reached.
It is a yet further object of the present invention to develop a shoulder fired weapon with sabot sections and to integrate the sabots with a shot start feature.
These and other objects, features and advantages of the invention will become more apparent in view of the within detailed descriptions of the invention, the claims, and in light of the following drawings wherein reference numerals may be reused where appropriate to indicate a correspondence between the referenced items. It should be understood that the sizes and shapes of the different components in the figures may not be in exact proportion and are shown here just for visual clarity and for purposes of explanation. It is also to be understood that the specific embodiments of the present invention that have been described herein are merely illustrative of certain applications of the principles of the present invention. It should further be understood that the geometry, compositions, values, and dimensions of the components described herein can be modified within the scope of the invention and are not generally intended to be exclusive. Numerous other modifications can be made when implementing the invention for a particular environment, without departing from the spirit and scope of the invention.
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While the invention may have been described with reference to certain embodiments, numerous changes, alterations and modifications to the described embodiments are possible without departing from the spirit and scope of the invention as defined in the appended claims, and equivalents thereof.
The inventions described herein may be made, used, or licensed by or for the U.S. Government for U.S. Government purposes.
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