1. Technical Field of the Invention
The invention is in the field of kinetic anti-projectile interceptor vehicles.
2. Description of the Related Art
Interceptors have been proposed to intercept and disable or destroy space-based or space-entering projectiles, for example ballistic projectiles such as intercontinental ballistic missiles. Such projectiles travel at very high rates of speed and have short travel times, making interception of them a difficult problem, one in which there is room for further improvements.
According to an aspect of the invention, a kinetic anti-projectile interceptor vehicle (kill vehicle) includes foam arms that extend from a body of the vehicle, to thereby increase the effective area for colliding with a projectile to be intercepted.
According to another aspect of the invention, a kinetic anti-projectile interceptor vehicle includes extendible foam arms that have solid material pieces in them.
According to yet another aspect of the invention, a kinetic anti-projectile interceptor vehicle includes extendible arms that include a shape memory foam.
According to still another aspect of the invention, a kinetic anti-projectile interceptor vehicle includes foam arms that are heated to extend them from a body of the vehicle.
According to a further aspect of the invention, a vehicle includes a body, and arms that are extendable from the body. Mechanical restraints hold the arms in place until the arms are extended.
According to a still further aspect of the invention, a method of intercepting a projectile includes heating foam arms to extend them radially from a body of an interceptor vehicle. Mechanical restraints may be used to hold the foam arms in a retracted condition while the foam arms are being heated. The heating may be electrical heating. Electrical heating may also be used to release the mechanical restraint. For example the mechanical restraint may include a fusible link.
According to another aspect of the invention, a kinetic interceptor vehicle includes: a body; and foam arms that are extendible radially outward from the body.
According to yet another aspect of the invention, a method of intercepting a projectile comprises: directing a kinetic anti-projectile interceptor vehicle toward the projectile; after the directing, deploying foam arms of the vehicle radially outward from a body of the vehicle; and after the deploying, impacting the projectile with at least one of the body or one or more of the foam arms.
To the accomplishment of the foregoing and related ends, the invention comprises the features hereinafter fully described and particularly pointed out in the claims. The following description and the annexed drawings set forth in detail certain illustrative embodiments of the invention. These embodiments are indicative, however, of but a few of the various ways in which the principles of the invention may be employed. Other objects, advantages and novel features of the invention will become apparent from the following detailed description of the invention when considered in conjunction with the drawings.
In the annexed drawings, which are not necessarily to scale:
A kinetic anti-projectile vehicle includes a body, and extendible arms that extend radially from the body. The arms include a foam material, such as a shape memory foam. The foam material may be heated to expand or deploy it, to return the foam material to its original or deployed shape from its packaged shape. The foam arms may be mechanically restrained whole being heated. An electrically-activated mechanism may be used to remove the mechanical restraint, to allow the arms to expand. The mechanical restraint may be removed by heating, for example including a fusible link or a shape memory material. The foam material arms may include solid material, either in the form of solid material particles, such as high strength particles, or in the form of supports or restraints in the foam material. The extension of the foam arms increases the effective area of the vehicle for impacting a projectile. Impact on the projectile from the body and/or one or more of the arms may be sufficient to destroy, divert, or otherwise disable the projectile.
Referring initially to
With reference now in addition to
As explained in greater detail below, the arms 20 may include a foam material 26, such as a shape memory foam, that is heated in order to provide a force for shape change, in order to extend the arms 20 from the body 22. The heating may be performed by electrical heating of the foam material 26. The arms 20 may be mechanically restrained during the heating, in order that all of the arms 20 deploy at the same time. The mechanical restraints may involve solid material restraints within the foam material, and/or mechanisms that release with an electrical switch, such as through electrical heating and/or severing of a fusible link.
The arms 20 may be made of the foam material 26, such as shape memory polymer foam. The arms 20 may have pieces of solid material, such as a high-density metal or alloy in them, in order to provide greater kinetic energy when one or more of the arms 20 impact the projectile 12.
The arms 20 may have a diameter on the order of about 10 cm, and may have a length in their extended configuration on the order of meters. It will be appreciated that the arms 20 require no additional structural support when included on a space vehicle, as there are no gravity effects or wind resistance to distort their shapes.
In the following discussion first a general overview is given of the steps of a deployment process for deploying the arms 20. Then a schematic block diagram is given as an overview of the parts of the vehicle 10 used in deploying the arms 20. Finally several embodiments are discussed for the configuration of the arms 20 and for parts used in the deployment and configuration of the arms 20. It will be appreciated that the specific embodiments discussed are only examples of a wide variety of possible configuration of the arms 20 and the structures used in deploying the arms 20. The various embodiments may be discussed below only with regard to certain notable details, and it should be appreciated that details from the various embodiments may be combined, where appropriate, with those of other embodiments of the invention.
The heating may be electric heating of the foam material 26. Electric current may be passed through foam material itself, or through electrically conductive resistive heaters or other elements, such as wires, that are located within the foam material 26. The heating of shape memory foam material causes the material to produce a force to move it toward its “remembered” shape. This may involve an increase of at least 300% in a dimension of the arms 20, for example lengthening the arms 20 by a factor of four or more (a strain of at least 300%). Heating of foam that is not shape memory foam may soften the foam, making it easier to expand.
It will be appreciated that the shape memory polymer foam would expand during the heating unless it was restrained during the heating process. It is desirable that the shape memory polymer foam be restrained during heating in order to prevent the arms 20 from deploying prematurely. Premature deployment while heating would have the potential to deploy different of the arms 20 at different rates. Such asymmetric deployment could cause unwanted course changes to the vehicle 10, due to the change of location of the center of mass of the vehicle 10. Therefore in step 56, after the heating of the foam material 26 in preparation for extending the arms 20, mechanical restraint on the foam material 56 is released. This allows the arms 20 to extend in step 58, putting the vehicle 10 into the arms deployed or extended configuration shown in
The release of the mechanical restraint may be an electrically-actuated or electro-optically-actuated release mechanism (which together are referred to herein as an electrically-actuated release mechanism, or simply a release mechanism). As one example, the electrically-actuated release mechanism may involve electrical heating of a fusible link to sever the link to release the mechanical restraint. The electrically-actuated release mechanism may involve use of a shape memory solid material, such as a shape memory alloy, that reverts to a previous shape upon electrical heating. Such a shape memory material element may be embedded in the foam material 26, and may serve as a heating element for heating the foam material. In one embodiment the shape memory material solid element may be subjected a relatively small current to provide heat for heating up the foam material, and then a sudden increase or burst of electric current to cause heating of the shape memory alloy solid material above a transition temperature that results in it producing forces tending to put it back into a previous (memory) shape. Other possible electrically-actuated release mechanisms include cutters driven by a pressurized gas and actuated electrically, for severing some part of a mechanical restraint, and explosive bolts.
A release mechanism 80 is coupled to the mechanically restraint system 74 to release the mechanical restraint 74 after the heating has been completed, or at another time when extension of the arms 20 is desired. The release mechanism 80 may be an electrically-actuated release mechanism that is coupled to the power source 78 for its operation. Alternatively the release mechanism 80 may have a separate power source. The release mechanism may be a part of the mechanical restraint 74, such as a fusible link. The release of the mechanical restraint 74 may allow the foam material 26 to extend under its own forces, such as forces from a shape memory polymer foam that has been heated above a transition temperature. The release may also cause an element within or coupled to the foam arms to provide a force to extend the arms 20.
It will be appreciated that the strap 110 may not have to have great strength to contain the foam material 26 during heating, as shape memory foam material may produce only small forces, albeit forces sufficient to extend the arm 26. It will also be appreciated that other mechanisms may be used for severing and releasing a strap, such as a cutting mechanism like a pressure-driven cutter. It will further be appreciated that it is possible for the strap 110 to serve as a heater for heating the foam material 26 while still restraining the foam material 26, as long as the electric current passed through the strap 110 does not result in heating that will soften or melt the fusible link 112.
The shape memory alloy member 120 may be used as a heater for heating the foam material 26 while the foam material is restrained. A relatively low current may be passed through the shape memory alloy member 120, sufficient for heating the surrounding foam material 26, but not so much as to trigger the shape memory properties of the member 120. When extension of the arm 20 is desired, an increased electrical current may be passed through the shape memory alloy member 120. This heating would be sufficient to trigger the shape memory properties of the member 120, causing the member 120 to revert to a previous shape consistent with extension of the arm 20, as shown in
It will be appreciated that many other types of mechanical restraint systems and configurations of mechanical restraint systems are possible.
Although the invention has been shown and described with respect to a certain preferred embodiment or embodiments, it is obvious that equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. In particular regard to the various functions performed by the above described elements (components, assemblies, devices, compositions, etc.), the terms (including a reference to a “means”) used to describe such elements are intended to correspond, unless otherwise indicated, to any element which performs the specified function of the described element (i.e., that is functionally equivalent), even though not structurally equivalent to the disclosed structure which performs the function in the herein illustrated exemplary embodiment or embodiments of the invention. In addition, while a particular feature of the invention may have been described above with respect to only one or more of several illustrated embodiments, such feature may be combined with one or more other features of the other embodiments, as may be desired and advantageous for any given or particular application.
Number | Name | Date | Kind |
---|---|---|---|
2559827 | Northrop | Jul 1951 | A |
3628352 | Stuemky | Dec 1971 | A |
3952662 | Greenlees | Apr 1976 | A |
5049591 | Hayashi et al. | Sep 1991 | A |
5082207 | Tulinius | Jan 1992 | A |
5181678 | Widnall et al. | Jan 1993 | A |
5194030 | LeBoeuf et al. | Mar 1993 | A |
5219162 | Orbanes et al. | Jun 1993 | A |
5662294 | Maclean et al. | Sep 1997 | A |
6264136 | Weston | Jul 2001 | B1 |
6705568 | Lee | Mar 2004 | B2 |
6834835 | Knowles et al. | Dec 2004 | B1 |
7728267 | Sanderson et al. | Jun 2010 | B2 |
7766274 | Jameson et al. | Aug 2010 | B1 |
7777165 | Sanderson et al. | Aug 2010 | B2 |
7832690 | Levine et al. | Nov 2010 | B1 |
7939178 | Sar et al. | May 2011 | B2 |
8016249 | Sar et al. | Sep 2011 | B2 |
20020195177 | Hinkley et al. | Dec 2002 | A1 |
20030036090 | Patil et al. | Feb 2003 | A1 |
20030126978 | Rastegar | Jul 2003 | A1 |
20040086699 | Schneider | May 2004 | A1 |
20050157893 | Pelrine et al. | Jul 2005 | A1 |
20050206096 | Browne et al. | Sep 2005 | A1 |
20070107189 | Prichard et al. | May 2007 | A1 |
20080004686 | Hunt et al. | Jan 2008 | A1 |
20080061192 | Sullivan | Mar 2008 | A1 |
20090072094 | Sanderson et al. | Mar 2009 | A1 |
20090131959 | Rolland | May 2009 | A1 |
20090206192 | Sanderson et al. | Aug 2009 | A1 |
20090286101 | Sar et al. | Nov 2009 | A1 |
20100030308 | Anderson et al. | Feb 2010 | A1 |
20100282917 | O'Shea | Nov 2010 | A1 |
20100288870 | Geswender et al. | Nov 2010 | A1 |
Number | Date | Country |
---|---|---|
101028866 | Sep 2007 | CN |
3116175 | Nov 1982 | DE |
0361418 | Apr 1990 | EP |
0905019 | Mar 1999 | EP |
1607602 | Dec 2005 | EP |
2445099 | Jun 2008 | GB |
60145385 | Jul 1985 | JP |
2009047179 | Mar 2009 | JP |
9308013 | Apr 1993 | WO |
9324300 | Dec 1993 | WO |
03068584 | Aug 2003 | WO |
2007001392 | Jan 2007 | WO |
2008068472 | Jun 2008 | WO |
Entry |
---|
“A study on processing of composite metal foam via casting”, A. Rabiei, A.T. O'Neill; Materials Science and Engineering A404 (2005) pp. 159-164. Jul. 25, 2005. |
“Shape Memory Polymer Characterization for Advanced Air Vehicle Technologies”, Raytheon Technology Today, (2007), vol. 2007, No. 4, [retrieved from internet] <www.raytheon.com/technology—today/archive/2007—issue 4.pdf>. |
Thill C. et al., “Morphing Skins”, Aeronautical Journal, (2008), vol. 112, No. 1129, [retrieved from internet], <www.aer.bris.ac.uk/research/fibres/morph%20pics/RoyAeroSocMorphSkin.pdf>. |
International Search Report and Written Opinion from corresponding International Application No. PCT/US09/54742. |
Shaw, John A. et al., “The Manufacture of Niti Foams”, Proceedings of 2002 ASME International Mechanical Engineering Congress and Exposition, (2002), pp. 1-10. |
Perkins, David A. et al., “Morphing Wing Structures for Loitering Air Vehicles”, 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, (2004), pp. 1. |
Number | Date | Country | |
---|---|---|---|
20120180691 A1 | Jul 2012 | US |