Any fault condition must be eliminated and the latched fault indication must
be cleared before power can be switched on to the unit under test. The BPU intentionally
does not have a remote control or external control interface. Not having a remote/external
control eliminates the chance that an erroneous or rogue command can inadvertently
apply power to the unit under test or change voltage thresholds. The BPU uses
comparator circuits to detect the fault conditions. The comparator outputs feed
a FPGA that implements logic functions and provides digital filtering. Recessed
trim pots set the comparator threshold levels from the front panel. The Over/Under/Reverse
thresholds can be displayed while adjustments are made. The BPU also incorporates
a separate crowbar circuit for additional over voltage protection. For battery
simulator applications, the 150A series diode can be jumpered across allowing
current to flow either direction.
The BPU is available with several options. One option includes a switched
AC outlet. The switched outlet can be used to power a large 'Spacecraft is
Powered' warning lamp or be used to power an elapsed counter. The elapsed
counter can be useful to keep track of burn-in time. Other options include
changing the circuit breaker size, changing the circuit breaker to a fuse,
a 120VDC version, additional auxiliary outputs, etc.
BPU Model
The
Bus Protection Unit (BPU) is a ground support element designed to protect a
spacecraft or flight box against wrong voltage levels during integration and
test. The BPU can detect an Over/Under/Reverse-Voltage Fault Condition. A BPU
will not switch on if a Fault Condition is present and will switch off if a
Fault Condition occurs after power is switched to the unit under test. The BPU
primarily protects against voltage faults but does include current protection
by way of a DC circuit breaker. The BPU must manually be switched on from the
front panel.