Selectable kinetic energy of projectiles
Projectiles with sealed propellant are described herein. In one embodiment of the invention, a projectile includes a body having a nose portion and a tail portion, a plurality of propellant charges contained within the body, a plurality of selectable initiators contained within the body for ignition of respective propellant charges, one or more ports for exit of ignition gases produced by the charges for propulsion of the projectile from the weapon, and one or more inductors for inducing a firing current, where at least one initiator only initiates on receiving a firing current which is different from the firing signal required to initiate the other initiators.
1. A projectile for a weapon, comprising:
a body having a nose portion and a tail portion;
a plurality of propellant charges contained within the body;
a plurality of selectable initiators contained within the body for ignition of respective ones of the plurality of propellant charges;
a port for exit of ignition gases produced by each of the plurality of propellant charges for propulsion of the projectile from the weapon; and
one or more inductors for inducing one or more firing currents, wherein at least one initiator only initiates on receiving a firing current of the one or more firing currents which is different from another firing current of the one or more firing currents required to initiate the other initiators.
2. A projectile as in claim 1 , wherein the one or more firing currents differ by energy level.
3. A projectile as in claim 1 , wherein the one or more firing currents are encoded and the projectile includes a decoder.
4. A projectile as in claim 3 , wherein the decoder includes logic circuits.
5. A projectile as in claim 3 , wherein the encoding comprises pulse width modulation, pulse code modulation or pulse amplitude modulation.
6. A projectile as in claim 1 , wherein the one or more inductors are coils.
7. A projectile as in claim 1 , comprising one inductor for each initiator.
8. A projectile as in claim 1 , wherein the initiators include semiconductor bridges and a set-up or booster pyrotechnic compound.
9. A projectile as in claim 1 , wherein each propellant charge has a port for exit of respective ignition gases.
10. A projectile as in claim 1 , wherein a single port is provided for exit of ignition gases from all of the propellant charges.
11. A projectile as in claim 1 , wherein the plurality of propellant charges are positioned so that one or more of the plurality of propellant charges closer to the port are positioned to be ignited by the ignition gases from a first ignited propellant charge positioned further from the port.
12. A projectile as in claim 1 , wherein the charges are distributed around a longitudinal axis of the body.
13. A projectile as in claim 1 , wherein the plurality of propellant charges are distributed along a longitudinal axis of the body.
14. A projectile as in claim 1 , wherein the nose and tail portions of the projectile are adapted respectively to fit tail and nose portions of adjacent leading and trailing projectiles in a stack.
15. A projectile as in claim 1 , further comprising a payload in the nose portion.