Energy beam interceptor
View Patent ↗Disclosed is an energy beam interceptor that includes an interceptor vehicle of either a missile or a lighter than air vehicle that carries an energy beam generator with a minimum power output of approximately 500 W, a high density power supply that power the energy beam generator, an energy beam targeting apparatus that directs emissions from the energy beam generator and an energy beam targeting controller that targets emissions from the energy beam generator with the energy beam targeting apparatus.
1. An energy beam interceptor comprising:
a missile;
an energy beam generator with a minimum power output of approximately 500 W, wherein the energy beam generator is mounted on the missile;
a high density power supply constructed and arranged to power the energy beam generator, wherein the high density power supply is mounted on the missile;
an energy beam targeting apparatus constructed and arranged to direct emissions from the energy beam generator, wherein the energy beam targeting apparatus is mounted on the missile; and
an energy beam targeting controller constructed and arranged to target emissions from the energy beam generator with the energy beam targeting apparatus.
2. The energy beam interceptor of claim 1 , wherein the missile has a payload capacity exceeding 300 lbs with a flight ceiling exceeding 250,000 feet.
3. The energy beam interceptor of claim 1 , wherein the energy beam generator has a minimum power output of approximately 3 kW.
4. The energy beam interceptor of claim 1 , further comprising a sensor configured to detect external electromagnetic signals.
5. The energy beam interceptor of claim 4 , wherein the sensor is selected from the group comprising: visible light sensor, radar receiver, laser receiver and heat sensor.
6. The energy beam interceptor of claim 4 , further comprising a targeting emitter.
7. The energy beam interceptor of claim 6 , wherein the targeting emitter is a radar emitter.
8. The energy beam interceptor of claim 1 , further comprising a recovery device constructed and arranged to safely deliver the energy beam generator to the earth after use.
9. The energy beam interceptor of claim 8 , wherein the recovery device and the energy beam generator are selectively separable from the missile.
10. The energy beam interceptor of claim 1 , further comprising a missile targeting controller constructed and arranged to control the flight path of the missile.
11. An energy beam interceptor comprising:
a lighter than air vehicle;
an energy beam generator with a minimum power output of approximately 500 W, wherein the energy beam generator is mounted on the lighter than air vehicle;
a high density power supply constructed and arranged to power the energy beam generator, wherein the high density power supply is mounted on the lighter than air vehicle;
an energy beam targeting apparatus constructed and arranged to direct emissions from the energy beam generator, wherein the energy beam targeting apparatus is mounted on the lighter than air vehicle; and
an energy beam targeting controller constructed and arranged to target emissions from the energy beam generator with the energy beam targeting apparatus.
12. The energy beam interceptor of claim 11 , wherein the energy beam generator has a minimum power output of approximately 3 kW.
13. The energy beam interceptor of claim 11 , further comprising a sensor configured to detect external electromagnetic signals.
14. The energy beam interceptor of claim 13 , wherein the sensor is selected from the group comprising: visible light sensor, radar receiver, laser receiver and heat sensor.
15. The energy beam interceptor of claim 13 , further comprising a targeting emitter.
16. The energy beam interceptor of claim 15 , wherein the targeting emitter is a radar emitter.
17. The energy beam interceptor of claim 11 , further comprising a recovery device constructed and arranged to safely deliver the energy beam generator to the earth after use.
18. The energy beam interceptor of claim 17 , wherein the recovery device and the energy beam generator are selectively separable from the lighter than air vehicle.
19. A method of intercepting an airborne target comprising:
launching a missile carrying an energy beam generator with a minimum power output of approximately 500 W, a high density power supply constructed and arranged to power the energy beam generator, an energy beam targeting apparatus constructed and arranged to direct emissions from the energy beam generator, and an energy beam targeting controller constructed and arranged to target emissions from the energy beam generator with the energy beam targeting apparatus;
identifying the target;
targeting the energy beam generator at the target; and
firing the energy beam generator at the target when the target is within one mile distance from the missile.
20. The method of claim 19 further comprising:
emitting radar energy from a targeting emitter on the missile:
detecting the radar energy with a radar receiver on the missile;
controlling the flight path of the missile with a missile targeting controller based at least in part on detected radar energy; and
targeting the energy beam generator at the target based at least in part on detected radar energy.