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Electromagnetic Space Drive

Inventor: Roger J. Shawyer
Device: EmDrive
Folder: shawyer
Original: Open article
Confidence
0.78
Practicability
0.45
Evidence
0.40
Fringe Score
0.85
Risk
0.10
TRL
5

Goal

Provide propellant-less thrust for satellite and spacecraft propulsion.

Problem

Heavy, limited-life propellant subsystems that increase launch mass and cost for space missions.

Concept Summary

The EmDrive uses a tapered, high-Q resonant microwave cavity. Microwave radiation is generated by a magnetron, circulates within the cavity, and, because of radiation pressure and differing phase velocities along the tapered waveguide, a net thrust is produced without expelling propellant.

Principles

  • Radiation pressure of electromagnetic waves
  • Newton's second law (force = rate of change of momentum)
  • Momentum of photons
  • Resonant cavity Q-factor amplification
  • Waveguide geometry affecting phase velocity
  • Special relativity (different reference frames for wave and cavity)

Scientific Domains

Physics Aerospace Engineering Electromagnetics

Materials

  • Copper or aluminum waveguide
  • Metallic reflectors (e.g., copper, aluminum)
  • Water-cooled magnetron
  • Ceramic insulating supports

Mechanisms of Action

  • Microwave energy is injected into a tapered resonant cavity.
  • The EM wave reflects between two metal reflectors, creating a pressure differential due to differing propagation speeds.
  • The high Q of the cavity amplifies the effect, resulting in a measurable net thrust along the axis of the cavity.

Energy Sources

Electrical power feeding the magnetron (microwave source)

Applications

  • Satellite orbit adjustment
  • Station-keeping
  • Deep-space probe propulsion
  • Reduced launch mass for satellites

Claimed Performance

Maximum specific thrust of 214 mN/kW measured in static tests; flight-model 300 W C-band thruster specified to produce 85 mN thrust.

Experimental Evidence

Static test rig with calibrated composite balance; 134 test runs; measured cavity Q ~= 45,000; thrust up to 214 mN/kW reported.

Replication Status

Demonstrated in internal static and dynamic test programmes; no independent third-party replication reported in the article.

Limitations

  • Lack of independent verification
  • Low thrust-to-power ratio compared with conventional electric thrusters
  • Thermal management of high-Q cavity
  • Potential scalability issues

Red Flags

  • Claims of propellant-less thrust contradict well-established physics.
  • No peer-reviewed, independently replicated experimental data presented.

Keywords

EmDrive microwave thruster propellantless propulsion radiation pressure high-Q resonant cavity

Related Technologies

Microwave resonant cavity Magnetron power source Satellite electric propulsion

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