Electrically initiated inertial igniters for thermal batteries and the like

1. An electrically initiated inertial igniter for a munition, the electrically initiated inertial igniter comprising:

an electrical energy harvesting device for generating a voltage over a duration of an acceleration of the munition;

a circuit powered by the electrical energy storage device for determining when the acceleration experienced by the munition is an all-fire condition; and

an electrically activated reserve battery at least partially activated by the electrical energy harvesting device when the circuit determines that the acceleration experienced by the munition is the all-fire condition to electrically initiate pyrotechnic materials at a specified time into a flight of the munition;

wherein the circuit having a sub circuit having at least a capacitor for directing a portion of the charge resulting from the voltage and duration to the capacitor, wherein the all-fire condition is determined based on both the voltage and duration generated by the electrical energy harvesting device and a predetermined accumulated voltage in the capacitor.

2. The electrically initiated inertial igniter of claim 1 , wherein the sub circuit further includes a draining element for draining any charge accumulated in the capacitor resulting from non-firing events.

3. The electrically initiated inertial igniter of claim 2 , wherein the draining element is a resistor.

4. The electrically initiated inertial igniter of claim 1 , wherein the electrical energy harvesting device is a piezoelectric generator.

5. The electrically initiated inertial igniter of claim 1 , wherein the circuit is capable of being programmed to predetermined all-fire requirements.

6. The electrically initiated inertial igniter of claim 1 , wherein the electrical harvesting device is configured to provide a voltage pulse to the electrically activated reserve battery to activate the electrically activated reserve battery.

7. The electrically initiated inertial igniter of claim 6 , wherein the electrically activated reserve battery is configured to initiate electrowetting upon activation by the electrical harvesting device.

8. The electrically initiated inertial igniter of claim 1 , wherein the electrically activated reserve battery at least partially provides power to a heating wire to initiate ignition in the pyrotechnic materials upon activation by the electrical harvesting device.

9. A method for electrically initiating an inertial igniter for a munition, the method comprising:

generating a voltage over a duration of an acceleration of the munition;

powering a circuit from the generated voltage for determining when the acceleration experienced by the munition is an all-fire condition;

electrically activating a reserve battery by the generated voltage when the circuit determines that the acceleration experienced by the munition is the all-fire condition;

electrically initiating pyrotechnic materials at a specified time into a flight of the munition at least partially using the reserve battery;

directing a portion of the charge resulting from the voltage and duration to a sub circuit having at least a capacitor; and

determining the all-fire condition based on both the generated voltage and duration and a predetermined accumulated voltage in the capacitor.

10. The method of claim 9 , further comprising draining any charge accumulated in the capacitor resulting from non-firing events.

11. The method of claim 9 , further comprising programming the circuit to predetermined all-fire requirements.

12. The method of claim 9 , wherein the electrically activating comprises providing a voltage pulse to the reserve battery.

13. The method of claim 12 , wherein the voltage pulse initiates electrowetting in the reserve battery.

14. The method of claim 9 , wherein the electrically initiating comprises at least partially providing power from the reserve battery to a heating wire to initiate the pyrotechnic materials.