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Guido FETTA Microwave Thruster [ Cannae Drive ]

Inventor: Guido Fetta
Year: 2014
Device: Cannae Drive
Folder: fetta
Original: Open article
Confidence
0.80
Practicability
0.40
Evidence
0.60
Fringe Score
0.90
Risk
0.20
TRL
4

Goal

Generate thrust without propellant by using a resonant microwave cavity

Problem

Eliminate the need for propellant in spacecraft, reducing launch mass and cost

Concept Summary

The Cannae Drive is a propellant-less electromagnetic thruster that uses a radio-frequency resonant cavity (~=935 MHz) to create an imbalance of radiation pressure inside the cavity. The asymmetric cavity design is claimed to interact with quantum-vacuum virtual plasma, producing a net unidirectional force measured in the tens of micronewtons.

Detailed Description

A conductive resonant cavity is excited with high-frequency RF power, establishing a standing electromagnetic wave. The cavity is deliberately axially asymmetric, causing a reduced reflection coefficient at one end plate. This creates a differential radiation pressure that, according to the inventors, results in a net thrust. NASA's Johnson Space Center tested two versions (one "null" device and one active device) on a low-thrust torsion pendulum in a stainless-steel vacuum chamber at ambient pressure. Measured thrust was 30-50 uN, well above the instrument's sub-10 uN sensitivity. The test campaign lasted eight days, with manual frequency control and verification using an RF load to rule out non-cavity effects.

Principles

  • Radiation pressure imbalance
  • Asymmetric resonant cavity design
  • Interaction with quantum-vacuum virtual plasma
  • RF standing wave generation

Scientific Domains

Physics Aerospace Engineering Electrical Engineering

Materials

  • Conductive metal (e.g., copper, aluminum)
  • Stainless steel (vacuum chamber)

Mechanisms of Action

  • Radiation pressure
  • Quantum vacuum interaction
  • Asymmetric reflection coefficient

Energy Sources

Electrical power RF microwave power (~935 MHz)

Applications

  • Satellite station-keeping
  • Deep-space propulsion
  • Spacecraft maneuvering

Claimed Performance

30-50 uN of thrust produced by a resonant cavity operating at ~935 MHz, measured with a torsion pendulum capable of sub-10 uN resolution.

Experimental Evidence

NASA Johnson Space Center's eight-day test campaign (August 2013) recorded 30-50 uN of thrust from two RF resonant cavity devices, including a 'null' device that was not expected to produce thrust. The results were obtained using a low-thrust torsion pendulum in a stainless-steel vacuum chamber.

Replication Status

Independent testing by NASA Johnson Space Center confirmed the production of measurable thrust from the Cannae Drive cavity.

Limitations

  • Very low thrust (tens of uN)
  • Requires precise RF frequency control
  • Experimental validation limited to laboratory tests
  • No peer-reviewed publication of underlying physics

Red Flags

  • Claims of quantum-vacuum interaction lack independent theoretical verification
  • Potential for measurement artefacts in torsion pendulum experiments
  • Limited peer-reviewed literature

Keywords

Cannae Drive microwave thruster propellant-less propulsion RF resonant cavity quantum vacuum radiation pressure

Related Technologies

EmDrive Q-Drive microwave resonant cavity thruster RF propulsion

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