Interceptor projectile and method of use
An interceptor projectile includes a deployable net that deploys during flight and wraps around an incoming projectile, such as a rocket propelled grenade (RPG). The net is initially in a tubular body of the interceptor projectile. Weights are attached to ends of the net with metal cables. A propellant is used to deploy the net from the tubular body and to deploy the weights at acute angles to the longitudinal axis of the interceptor projectile. The weights move radially out from the interceptor projectile, expanding the net outward, and wrapping the net around an incoming projectile. The engagement of the net with the incoming projectile disables the incoming projectile, sending the incoming projectile off course.
1. A weapon interceptor projectile comprising:
a tubular body;
a net inside the tubular body;
weights attached to cables that are attached to the net;
a propellant operatively coupled to the net and the weights and the net, for deploying the weights and the net; and
a net piston inside the tubular body, between the net and the propellant, with the piston attached to the net; and
wherein the net piston is propelled out of the tubular body along with the net, to deploy the net.
2. The projectile of claim 1 , wherein the net piston includes fiberglass wadding.
3. A weapon interceptor projectile comprising:
a tubular body;
a net inside the tubular body;
weights attached to cables that are attached to the net; and
a propellant operatively coupled to the net and the weights and the net, for deploying the weights and the net;
wherein the cables run along an outer surface of the tubular body.
4. The projectile of claim 3 , further comprising a base that has angled holes in which the weights rest prior to deployment.
5. The projectile of claim 4 , wherein the holes make an acute angle with a longitudinal axis of the interceptor projectile.
6. A method of defending against an incoming projectile, the method comprising:
firing an interceptor projectile toward the incoming projectile;
after the firing, deploying a net and weights of the interceptor projectile; and
wrapping the net around the incoming projectile;
wherein the deploying includes igniting a propellant operatively coupled to the net and the weights, thereby separating the net and the weights from a body of the interceptor projectile;
wherein the separating includes moving the weights at an acute angle relative to a longitudinal axis of the interceptor projectile;
wherein the interceptor projectile includes a piston attached to the net by a tether; and
wherein the separating includes moving the piston substantially along the longitudinal axis of the interceptor projectile.
7. The method of claim 6 , wherein separating further includes rotating the weights about the piston as the piston moves.
8. The method of claim 6 ,
wherein the propellant includes:
a weight propellant charge operatively coupled to the weights for deploying the weights; and
a net propellant charge operatively coupled to the net for deploying the net;
wherein the propellant charges are in respective propellant chambers;
wherein the propellant chambers are in communication with one another; and
wherein the deploying includes igniting both of the propellant charges using an initiator of the interceptor projectile.
9. The method of claim 6 , wherein the wrapping includes the weights moving ends of the net, distal from a center of the net, around the incoming projectile.
10. The method of claim 6 , wherein the deploying includes propelling both the net and the weights toward the incoming projectile.
11. The method of claim 10 , wherein the propelling includes rotating the weights about a center of the net as the net and the weights move toward the incoming projectile.
12. The method of claim 6 , wherein the deploying includes using the propellant to move the weights faster than a center of the net.
13. The method of claim 12 ,
wherein the propellant includes:
a weight propellant charge operatively coupled to the weights for deploying the weights; and
a net propellant charge operatively coupled to the net for deploying the net; and
wherein the deploying includes using the weight propellant charge to move the weights faster than the net propellant charge moves the center of the net.