Arc flash microwave rocket experiment

Title: Exploring Thrust Generation in an Experimental Rocket Motor Using Arc Flash, Microwaves, and Magnetic Fields

Abstract:

This theoretical paper investigates the potential of a novel propulsion system designed as an experimental rocket motor. The prototype incorporates a combination of arc flash, microwaves, and magnetic fields to induce a unique propulsion mechanism. The theoretical foundation of this propulsion system lies in the expansion of metal-based fuel into a gas and subsequently a plasma state, generating sufficient energy and force for lift.

Methodology:

The combustion chamber was constructed with a copper rod, an aluminum rod, and sheet steel forming the top, wherein the metal-based fuel sample was placed. The chamber included an opening for microwaves and a 40-45% angled configuration to facilitate efficient gas expansion. The nozzle featured a shrinking cone design, surrounded by a double-wrapped electromagnetic coil composed of an 8-inch iron pipe with high-amp wire.

Experimental Setup:

The arc flash, generated by a modified welder, was synchronized with the magnetic field and microwaves using a direct connection to the household breakers. A dial switch controlled the power to the microwave transformer. Observations revealed an anticipated reaction, but the engagement of microwaves resulted in an elevated response. As power levels increased, so did the observed thrust and accompanying sound, reminiscent of a jet engine.

Results:

The experiments demonstrated potential thrust generation, with noticeable reactions indicating the feasibility of the proposed propulsion system. Subsequent prototype iterations with a fuel feeding system showed promise, although limitations arose with stationary fuel sources. The need for a stronger microwave emitter or multiple emitters led to challenges in frequency modulation to avoid wave neutralization.

Discussion:

The study suggests that scaling up the magnetic field and optimizing microwave emission could enhance thrust generation. The observed effects hold promise for applications in zero gravity environments and potentially atmospheric flight. Further research is warranted to address challenges related to fuel source mobility, frequency modulation, and scalability of magnetic components.

Conclusion:

This theoretical exploration of an experimental rocket motor incorporating arc flash, microwaves, and magnetic fields reveals promising avenues for thrust generation. The observed reactions and unique propulsion mechanism open the door to further investigations and potential advancements in aerospace technology.