Inductive resistance influence on functioning of thrust module simulator V.A.Lesnevskiy, V.V.Sokolov EDB "Fakel" EDB Fakel develops and manufactures electric
propulsion systems (EPS). EPS is a complicated functional system which consists
of a stationary plasma thruster (SPT), xenon flow controller (XFC), propellant
storage and supply system (SSS), and power processing unit (PPU). PPU generates the required modes of electric power
supply for all the elements that constitute EPS, either of which differs in a
mode and consumed power, as well as in the nature of processes that run in the
paths of power transmission. In this connection, for each type of EPS consumers
it is necessary to create generators of the required mode of electric power
supply and separate paths of power transmission in PPU. Also, PPU provides
receipt and operation of coming control commands from the on-board digital
computer complex of a spacecraft (S/C), generation and transfer of telemetry
information to the telemetry control system [[1]]. To perform autonomous tests and
incoming inspection of PPU at the enterprise-manufacturer of EPS, it is
necessary to develop an electrodynamic thruster
simulator (EDTS) that simulates functioning of SPTs and EPS elements as a whole
at different operation modes. To provide high integrity of the data obtained
during the activities with EDTS, rather severe requirements for static and
dynamic accuracy of EPS simulation are placed on the articles of this type.
Dynamic characteristics are specified as frequency responses of internal
impedance of EDTS module. EDB Fakel has developed a simulator that consists of
the following simulative units [[2]]: - discharge gap simulator; - magnetic system simulator; - simulator of cathode-compensator heaters (SoCCH); - XFC simulator; - ignition discharge simulator. During the incoming inspection of the PPU manufactured
by OJSC AVEKS for КazSat, Express-MD S/Cs
using EDTS the measured value of the cathode heater current turned out to be above normal. Since the PPU supplied a.c. to the
cathode heater, additional inductive resistance emerged in the SoCCH of EDTS. This
work presents the influence of inductive resistance of the line and transformers
on the impedance of SoCCH, the assessment of influence of the higher harmonic components on a value of the actual current that passes
though the heaters. The feature of SPT as an object of power supply is a
high consumed power (up to 50% of the power generated aboard the S/C) and
multi-channeling of electric power consumers. The main elements of SPT power
supply are: anode, heater of the cathode, igniter, magnetic coils and thermothrottle. SPT consists of two plasma cathode-compensators which
contain the heaters designed for the startup heating. The simulator of
cathode-compensator heaters simulates their resistance that several times
increases while heating. The possibility of manual regulation of heaters
resistance is provided for. It follows from an analysis that to decrease output
impedance it is necessary to decrease internal impedance of the power amplifier,
increase amplification factors and to extend frequency band of the operational
amplifier, power amplifier and voltage amplifier. Measurements of leakage inductance of the transformers
were made due to the decrease of reactance of the line during the incoming
inspection of the PPU, which transformers are intended to correlate input
circuits of the cathode heater simulators with the load unit in EDTS. Additionally, inductive resistances of double-wire
lines of These tests were carried out to determine the
influence of inductive resistance of the lines and transformers on impedance of
the cathode heater simulators in the electrodynamic simulator of thrust module. As a connecting line the following options were
considered: - non-twisted parallel wires; - twisted wires; - insulated wire pulled into the braid shielding ПМЛ, where the shielding functioned as a current-carrying
return wire. - parallel connection of two lines of the wire in the
braid shielding ПМЛ. Due to deep influence of relative position of the
wires in a pair of two non-twisted wires, the inductance of the lines was taken
as a mean value of the seven measured - 0.53 μH. For the lines, the МГШВ wire with a cross section of 1 mm2 was
used. To determine total/accumulative leakage inductance of
the transformer windings we relied on the fact that in the event of a
short-circuit of the transformer secondary winding, its primary winding
represents inductance that is equal to the sum of leakage inductance of the
primary winding and leakage inductance of the secondary winding reduced to the
primary one. To measure inductances, a resonance method was used,
where a condenser is connected to the in-parallel sought inductance, and then
sine voltage is supplied to the resulting parallel oscillating contour. The
equality of environmental expose frequencies and contour eigen frequency leads
to the increase of amplitude of oscillations in it, what is recorded by an
electron oscillograph. Noticeable differences in a value of leakage
inductance of transformer #3 are caused by a change in the technique of winding
insulation manufacture, and of transformer #5 - by particular thoroughness of
performance of all the operations related to the manufacture. To calculate inductive
resistance of the heater circuits simulators of EDTS, the sum of the
transformer leakage inductances and different option line inductances is taken.
That the increase of the
cathode heater simulator impedance in EDTS due to inductive resistance of the
transformers and supply line is: - approximately
0.28% in the best case when the line of the wire pulled into the braid
shielding ПМЛ is used, −
~ 1% in the worst case when the line of twist-free wires is used. Given that the higher
harmonic components of oscillations are several times lower than the value of
the first harmonics with their amplitudes decaying while the harmonic number
grows, the influence of the higher harmonic components of oscillations is much
lower than that of the first harmonics. Therefore, the reactive
component of the cathode heater simulator impedance in EDTS does not
significantly influence the value of a current that passes through it. To
exclude the reactive component of the simulator resistance, the supply lines in
EDTS should be made of a twisted wire which represents a wire pulled into the
braid shielding ПМЛ,
where the braid should be used as a current-carrying return wire. [1] M.V.
Mikhailov. Power processing unit of the stationary plasma thruster. Thesis work
to get the academic title of the Doctor of Science. The [2] V.A.
Lesnevskiy, A.V. Rumyantsev, V.V. Sokolov. Simulator of electrodynamic
characteristics of the thrust module. Herald of the |
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