• Home
  • Current congress
  • Public Website
  • My papers
  • root
  • browse
  • IAC-18
  • C4
  • 7-C3.5
  • paper
  • SpaceDrive – Thrust Balance Development and First Measurements of Mach-Effect and EMDrive Thrusters

    Paper number

    IAC-18,C4,7-C3.5,5,x46021

    Author

    Prof. Martin Tajmar, Germany, TU Dresden

    Coauthor

    Mr. Matthias Kössling, Germany, TU Dresden

    Coauthor

    Mr. Maxime Monette, Germany, TU Dresden

    Coauthor

    Mr. Marcel Weikert, Germany, TU Dresden

    Year

    2018

    Abstract
    Forces claimed by potential propellantless propulsion systems like the Mach-Effect thruster, developed by Prof. Woodward, and the EMDrive, developed by R. Shawyer, are in the µN or even sub-µN range. Within the framework of our SpaceDrive project, an automated thrust balance design capable of measuring forces of at least 100 nN for thrusters and their electronics with a mass up to 10 kg is described. The torsion balance features two different calibration methods, adjustable magnetic damping and tilt control as well as electromagnetic shielding. All onboard electronics can be controlled wirelessly via an infrared module for serial communication or via a laser module for fast Ethernet communication. Power is supplied to the balance using three separate liquid metal feedthroughs: one for voltages of 500 V and frequencies up to 200 kHz, one for high voltage up to 30 kV DC or AC, and one for high frequency signals around 3 GHz. The thruster can be rotated up to 180° to measure different thrust directions without breaking the vacuum and changing the setup in order to gain confidence and refute e.g. thermal drifts. The whole balance is controlled via a script language implemented in Labview. Calibration, noise and force measurements for both Mach-Effect as well as EMDrive thrusters are shown and discussed.
    Abstract document

    IAC-18,C4,7-C3.5,5,x46021.brief.pdf

    Manuscript document

    IAC-18,C4,7-C3.5,5,x46021.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.