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Future NASA missions will require high-performance electric
propulsion systems. Hall thrusters like the NASA-457M and the NASA-400M are
being developed at NASA Glenn Research Center (NASA GRC) for high-power,
high-specific impulse operation. These thrusters operate at power levels up to
50 kW of power and discharge voltages in excess of 600 V. A parallel effort is
being conducted to develop power electronics for these thrusters that push the
technology beyond the 5 kW state-of-the-art power level.
PPUs for high power systems challenge current technology. High voltages and
currents require special attention so that undesirable power losses and
parasitic transients are not created. For high power applications, power can be
processed in smaller fractions to reduce voltage and current magnitudes and
allow the use of more efficient semiconductors. These power modules can be used
as building blocks by connecting them in series or parallel to produce the
desired voltages and currents.
Recently NASA GRC developed a 1 kW power module for Hall thrusters, shown in
Figure 1. It consisted of a phase-shifted full-bridge converter operating at a
switching frequency of 50 kHz. The module, operated with an input voltage of 100
± 20 VDC, generated a nominal output of 300 VDC. This module, integrated with a
NASA-120Mv2 HET, demonstrated efficiencies in excess of 96 percent. The total
component weight of this unit, including printed circuit boards, was 0.765 kg.
The reason for developing this module was to create a test bed to evaluate
circuits, concepts and designs that could be applied to a higher power module
design.
The 1 kW power module was not designed with circuitry to operate multiple
modules in a parallel configuration. During this investigation, a load current
share circuit was designed and implemented to force the output current to evenly
divide between modules. Three 1 kW modules were connected in an arrangement with
both inputs and outputs in parallel to increase current output. In addition,
this parallel arrangement enabled the use of a phase-synchronization or
phase-staggering circuit that shifted the switching phases of the modules
reducing input and output ripples. Three 1 kW modules including these additional
functions were used to assemble a 3 kW discharge power supply. This unit was
successfully integrated with the NASA-120Mv2 HET.
All power and control design concepts implemented in the 1 kW module were
then used to develop a multi-kilowatt power module. A power level of 10 kW was
selected because of semiconductor parts and magnetic cores availability. The
topology used for the 10 kW module was also a phase-shifted full-bridge
converter. Three significant design changes had to be implemented relative to
the 1 kW design because of the higher power level on this application. First,
the switching frequency was decreased from 50 kHz to 20 kHz to reduce switching
losses. Second, the power stage that routes input current through the MOSFETs
and the transformer was designed to minimize interconnections, current path
length and loop inductance. These can introduce parasitic elements to the power
circuit resulting in transients detrimental to the performance of a converter.
Snubbers are then required to damp these transients at the cost of further power
losses. The power stage also included larger heat sinks for improved heat
rejection. Third, the gate drive circuit design was changed from a charge-pump
based circuit to a transformer-isolated design with high current drivers. This
was implemented because the larger gate capacitance in high power transistors
requires high current for fast and efficient switching. The bipolar drive from
the transformer-isolated design improves turn-off characteristics. In addition,
a "Miller killer" circuit, using a bipolar junction transistor, was
added to minimize the effect of the Miller capacitance on the MOSFETs and
further increase turn-off speed.
Other changes were made to improve efficiency. Two high-power MOSFETs, in an
SOT-227 package and with very low on-resistance, were used on each leg of the
bridge converter. Also, high-voltage, high-current, ultra-fast, soft-recovery
diodes, in a TO-247 packages, were used for the output rectifier. These allowed
the use of one single bridge rectification output stage, which minimizes losses
and simplifying transformer design. Last, a new high power transformer was
assembled by stacking two large ferrite C-cores. The windings utilized an
interleaved design, a minimum number of layers and Litz wire to minimize leakage
inductance and proximity and skin effects.
As in the 1 kW module design, phase-shifted, peak-current-mode,
pulse-width-modulation (PWM) control was implemented using a commercially
available integrated circuit (IC). This device included all the necessary
functions including the four phase-shifted gate drives, current limit and
soft-start. Integrating this IC into the design resulted in a significant part
count reduction. The component weight of the 10 kW power module is 6.2 kg not
including heat sinks or mounting hardware. A photograph of the breadboard is
shown in Figure 4.
The performance of the multi-kilowatt power module was tested using a
resistive load. Efficiencies greater than 96 percent were obtained through a
wide range of output powers. These efficiencies were attributed to the
soft-switching characteristics of the phase-shift bridge converter, fast gate
drive circuits and low parasitics losses inherent in the design.
This 10 kW power module will be used to develop a discharge supply for
high-power HETs. As proven with the 1 kW module, multiple units will be
connected in parallel to scale the design to high power.
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