In 2009 and 2010, Brito, Marini and Galian published a noteworthy experiment with negative results regarding Woodward's theory and a particular design of EM thrusters. Brito et. al.'s experiment had the ability to discriminate between thrusts in the uN (microNewton) range while the predicted Woodward thrust was 3.4 mN (milliNewton), orders of magnitude larger, yet the results showed no measurable thrust. These are the experimental reports:
2009, Hector H. Brito, Ricardo Marini and Eugenio S. Galian, "Null Findings on Electromagnetic Inertia Thruster Experiments using a Torsion Pendulum" 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2 - 5 August 2009, Denver, Colorado
http://enu.kz/repository/2009/AIAA-2009-5070.pdf2010, Ricardo L. Marini; Eugenio S. Galian , "Torsion Pendulum Investigation of Electromagnetic Inertia Manipulation Thrusting" Journal of Propulsion and Power, Vol. 26, No. 6 (2010), pp. 1283-1290
http://arc.aiaa.org/doi/abs/10.2514/1.46541?journalCode=jpp
Quoting from their report:
<<The thruster, is a self-contained unit including the propulsion modules and a battery operated 600W/1MHz power processing unit (PPU). Each module comprises a 30 turns toroidal coil wrapped around a ceramic housing containing a 10 nF - 8 mm wide annular capacitor with BaTiO3 ceramic dielectric (epsilonr ~ 4400). The capacitor-coil assembly is wired as a tank circuit and mounted in a common acrylic housing filled with a Phase Change Material (PCM), for limited thermal control of the assembly. The modules are wired in parallel to a common supply of 350 V- AC @ 1 MHz>>
<<For direct assessment of propulsive forces, a Cavendish-Coulomb method of detection based on a very sensitive single fiber torsion pendulum was implemented, together with a Kelvin laser measurement technique (see Fig. 4). ... The test unit being a self-contained one, spurious effects like inner motions, selfelectromagnetic couplings, piezoelectric, electro/magnetostriction, and thermal shifts of center of mass, are deemed to have a negligible influence on the setup dynamics. The thruster and its counterweight are fixed to a hollow cylindrical bar 0.4-m length, the whole fixture vertically suspended by a steel wire 0.8-mm dia., 2.45-m length. The suspension point was located 0.22 m from the thruster center of mass, and 0.15 m from the counterweight attachment point. The suspended fixture had a moment of inertia with respect to the wire axis of 0.937 kg-m2, and a free oscillation period of 168 s. A laser beam is reflected by a mirror fixed to the suspension wire onto a screen located 5.02 m from the suspension. The successive peak locations of the laser dot are marked on the screen following visual recording of the dot, thus performing a Kelvin laser measurement technique.>>
<<After conducting setup dynamics simulations involving varied initial conditions as well as activation times (t2 – t1), the setup was found to be able of discriminating thrusts in the N (microNewton) range, when the forces were applied according to the above mentioned procedure. However, under activation of the RAMA-II thruster in non-modulated power mode, no propulsive effect above that sensitivity range was observed, as shown in Table 1 where three successive peak locations are presented for each test, with the thruster activation occurring between peaks #2 and #3. In all tests two propulsive modules of four were activated to avoid PPU overheating and the measured supply voltage was 280 V, which yields an expected thrust around 320 mN, according to Eq. (1). Lower than nominal PPU output voltages were reported as related to poor current delivery capabilities of the employed lead-acid batteries, and built in current and temperature limitations to avoid propulsion modules and PPU overheating.>>
<<
The observed negative results for [Brito's EM drive] activation in non-modulated power mode, imply that the following theoretical approaches are wholly or partially falsified: Transient mass fluctuation, Thrust predicted according to Woodward’s formulation is around 3.4 mN, thus according to the results reported here no Mach induced mass fluctuation is taking place up to the sensitivity of the experimental apparatus.>>