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The maximum thrust of 5.3 mN could be obtained at 71 kHz with 70 Vpp.
Just over two minutes later, after reaching a maximum thrust of 3.6 million pounds, the motor exhausted the fuel and fell quiet.
The thrust forces and moment are determined by the maximum thrust of the thrusters as well as the thruster configuration.
Sonic combustion was autonomously realized in the combustor, resulting in delivery of a maximum thrust of 2250 N in the stoichiometric condition.
In load capacity test, the maximum thrust of the motor is about 10.01 N measured by adding different external loads on the mover.
The numerical results gave a maximum thrust of 3840 mN, and a total impulse of 0.42 mNs at the local ignition model.
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Optimization of fuels for the maximum thrust to drag ratio or specific impulse must consider the linkage of geometric restraints on the selection of fuel materials.
Experiment results show that a maximum no-load speed of 621 mm/s, a maximum thrust force of 11 N, and a maximum power of 1.9 W are achieved by the prototype.
The prototype achieved a maximum speed of 350 μm/s at a voltage of 400 Vp-p and frequency of 250 Hz, and it achieved a maximum thrust force of 5.88 N at a preload of 63 N.
Experimental results show that the prototype has a mechanical resolution of 0.02 μm, yaw error less than 2 μm and maximum thrust force of 30N.
Furthermore, the overall and maximum thrust performance of blades with a modified trailing edge was shown to exceed those of blades with a wave-like leading edge, due to a shift in the location of the vortices by the induced flow.
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