초록 ▼

A selectable mode multi-mode missile carrying submunitions and incorporating guidance and target seeking functions includes triggering or actuation of the submunitions by programming function on the ground or on board another weapon platform or via a link from the ground or said the weapon platform.

A selectable mode multi-mode missile carrying submunitions and incorporating guidance and target seeking functions includes triggering or actuation of the submunitions by programming function on the ground or on board another weapon platform or via a link from the ground or said the weapon platform. The submunitions may also be actuated by an impact function. The programming function incorporates or interacts with mode determining or setting devices that cause the missile and its submunitions to selectively operate either in a penetrator mode, a distributed penetrator mode, or in a separation mode. The submunitions are actuated independently, in sequence, or in common with each other depending upon the operating mode selected.

대표청구항 ▼

We hereby claim and desire to secure by Letter Patent the following: 1. A multi-mode missile, comprising: a plurality of submunitions; a mode setting device which sets an operating mode of the plurality of submunitions contained in the multi-mode missile to selectively be in one of a penetrator mod

We hereby claim and desire to secure by Letter Patent the following: 1. A multi-mode missile, comprising: a plurality of submunitions; a mode setting device which sets an operating mode of the plurality of submunitions contained in the multi-mode missile to selectively be in one of a penetrator mode, a distributed penetrator mode, or a separation mode, wherein, in the penetrator mode, the plurality of submunitions are essentially conjoined in a common triggering arrangement, wherein, in the distributed penetrator mode, the plurality of submunitions are subjected to a relatively minor dispersion with respect to each other and are actuated in sequence as a penetration of a target comprising plural confined spaces progresses, wherein, in the separation mode, the plurality of submunitions sequentially leave the missile in a relatively large dispersal pattern and are thereafter individually actuated by a plurality of associated fazes each selected from the group consisting of an impact fuze, a proximity fine, and a time fine; one or more triggering devices which detonates one or more of the plurality of submunitions; and means for programming the mode setting device, wherein the means for programming the mode setting device receives an actuation signal via a communications link. 2. The missile of claim 1, further comprising means for dispersing the plurality of submunitions when the separation mode is set. 3. The missile of claim 1, wherein the plurality of submunitions are actuated by an impact fuze. 4. The missile of claim 1, wherein the plurality of submunitions are actuated by a proximity fuze. 5. The missile of claim 1, wherein the plurality of submunitions are actuated by a time fuze. 6. The missile of claim 1, wherein the means for programming the mode setting device interacts with the mode setting device which dependent on at least one manual or automatic actuation, cause the missile and the plurality of submunitions to operate in the penetrator mode in which the plurality of submunitions are conjoined and commonly triggered. 7. The missile of claim 1, wherein the distributed penetrator mode is suitable for actuation against a target comprising plural confined spaces, wherein the plurality of submunitions are sequentially triggered in various ones of the plural confined spaces of the target during penetration of walls, ceilings, or floors of the confined spaces by the multi-mode missile. 8. The missile of claim 1, wherein the penetrator mode is suitable for actuation against a precision target in which a target penetration is an objective. 9. The missile of claim 1, wherein the means for programming the mode setting device interacts with the mode setting device dependent on at least one manual or automatic actuation to cause the missile and the plurality of submunitions to operate in the separation mode in which the plurality of submunitions sequentially leave the missile and thereafter are each actuated by associated individual triggers, each of the associated individual triggers being either independent from or coordinated with the associated individual triggers of the other submunitions. 10. The missile of claim 1, wherein the mode setting device is arranged, dependent on a further actuation, to enable the plurality of submunitions to operate in the distributed penetrator mode in which the plurality submunitions achieve a minor sequential dispersion relative to each other and are actuated as target penetration by the missile progresses. 11. The missile of claim 1, wherein the separation mode is suitable for actuation against a dispersed target. 12. The missile of claim 1, wherein the submunitions are conjoined by a retentive tubular body comprising a plurality of parts joined together with each other in both the penetrator mode and in the separation mode until a dispersal point is reached in the separation mode. 13. The missile of claim 1, wherein, when the plurality of submunitions are in the penetrator mode and after a target is penetrated, the one or more triggering devices are programmed to detonate the plurality of submunitions after penetration is achieved. 14. The missile of claim 1, wherein, when a target impact is achieved without a complete target penetration, the one or more triggering devices are programmed to detonate the plurality of submunitions in conjunction with the target impact. 15. The missile of claim 1, wherein the plurality of associated fuzes are independently triggered. 16. The missile of claim 1, wherein the plurality of associated fuzes are commonly triggered. 17. The missile of claim 1, wherein the plurality of associated fuzes are sequentially triggered.