Launch
Position
Effect
This
set of experiments looks at how the launch start position affects
the muzzle velocity and corresponding efficiency.
Firstly
let us define the 'launch position '.
Refering to fig 1 we define the launch position
as the distance between the leading face of the projectile and the
rear face of the coil. The sign convention for delta is such that
when the leading face of the projectile is outside the rear of the
coil, delta is negative.

Fig
1.
The
energy source used in these experiments comprises several different
capacitors as detailed in table 1. Note that the third capacitor
in these experiments consists of two of the 6,800 uF capacitors
connected in parallel. The coil employed throughout the tests is
detailed in table 2. The test setup is shown diagrammatically in
fig 2. The delta-peak
trigger uses the optical sensor to control the turn off point
while allowing the launch position to be varied. The
power MOSFET module consists of eight IRF3415 devices connected
in parallel giving a pulsed current capability of around 800 A (based
on a half-sine pulse of ~4 ms). These are switched via an MC34152
MOSFET driver. A 10 m
current sensor is connected in series with the discharge current
path allowing the coil current to be recorded up to the point of
turn off.

Fig
2. General test setup.
It
should be noted that the positioning of the current sensor causes
a reduction in the MOSFET G-S voltage proportional to the sensor
current (10_mV/A). The nominal G-S
drive voltage is therefore set high enough such that the minimum
G-S voltage is at least 10 V. The MC34152 can be operated with supply
voltages up to 18 V. The sensor current isn't a parameter of particular
interest, but the current traces do provide information on the pulse
width. The reason for placing the current sensor in this location is that 'accidents'
are less likely when the measuring equipement is connected to the
system ground potential. The current sensor also reduces
the maxumum possible efficiency since it comprises a significant
fraction of the overall circuit resistance.
Manufacturer |
Panasonic |
BHC-Aerovox |
BHC-Aerovox |
Type |
GAA |
ALS-40 |
ALS-30 |
Can
Size |
77
Dia x 106 |
66
Dia x 106 |
36
Dia x 106 |
Rated
Voltage (V) |
50 |
63 |
100 |
Capacitance
(F) |
150,000
u |
33,000
u |
6,800 u |
ESR
(100 Hz) ( ) |
4.7
m |
8
m |
23
m |
Table
1. Capacitors used in tests.
Length |
Ro |
Ri |
|
Turns |
Res |
Ind |
27 |
18 |
7 |
1.8 |
~80 |
~45
m |
~76
uH |
Table
2. Coil Parameters.
The
natural response of the system for each capacitor is shown in fig
3.

Fig
3. RLC behaviour with different capacitors.
Results:
150,000
uF
33,000
uF
13600
uF
Conclusions
Last
Modified: 13 Feb 2004
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