TM 55-1520-240-23-10
16-48
FLARE DISPENSER SYSTEM
16-48
DESCRIPTION
The Flare Dispenser System is a countermeasure
to infra-red guided heat-seeking missiles when the
helicopter is airborne. The heart of the system is a
flare dispenser assembly, consisting of a dispenser,
electronics module, and payload module. Other
components are a remote test panel, timer, cockpit
control panel, six firing switches, and a safety relay. The
system is operated by 28 vdc.
NO BREAK - WORK HARDER
When a missile launch is detected, either by sight or
radar warning, the system is activated by pressing one
of the six firing switches. There are four firing switches in
the cabin and one on each cyclic stick control grip. Each
time any of the firing switches is pressed, the system
will fire a flare. If the switch is held down, the timer will
cause a flare to be fired every 2.5 seconds.
NO BREAK - WORK HARDER
The payload module has provisions for 30 flares. A
digital counter on the dispenser control panel indicates
the number of flares remaining. The panel also has a
RIPPLE FIRE switch, which jettisons all remaining flares
in case of an emergency, and an ARM/SAFE switch to
arm the system in flight.
NO BREAK - WORK HARDER
The electronics module programs the number of flares
to fire on each firing order. It also has a safety switch to
prevent accidental firing. This switch is activated by a
safety pin which is removed before flight and installed
immediately after landing.
NO BREAK - WORK HARDER
When the helicopter is on the ground, a proximity
switch on the aft landing gear disarms the system
by deenergizing a safety relay in the circuit. The
NORMAL/BYPASS switch stays in the NORMAL position
until moved to BYPASS for ground testing. In this mode,
the switch bypasses the landing gear switch to energize
the safety relay. Two caution lights on the panel indicate
a READY TO FIRE status and the landing gear switch
status.
NO BREAK - WORK HARDER
The CHAFF utility mode of the system is not used on
the CH47 helicopter.
THEORY OF OPERATION
Power for the flare dispenser system is provided by 28
vdc from the No. 1 dc bus through the CHAFF circuit
breaker on the No. 1 power distribution panel. The
system is readied for operation by setting the toggle
switch on the cockpit control panel to ARM.
NO BREAK - WORK HARDER
If the helicopter is on the ground, safety relay 147K1 will
be held deenergized by landing gear switch 148K2 and
the system will remain disabled. When the helicopter is
in the air, the switch closes, energizing the relay and
allowing power to flow to the remote test panel and
the cockpit control panel. With the safety pin removed
from the electronics module and the test panel switch at
ARM, the timer circuit is armed and lights on the test
panel come on to indicate that the landing gear switch is
closed and the system is armed and ready to fire.
NO BREAK - WORK HARDER
When a cockpit or cabin firing switch is pressed, a
28-volt firing signal is routed through the timer to the
flare dispenser. A flare from the payload module is
fired and the READY TO FIRE light on the remote test
panel goes out. A flare sensor in the dispenser checks
for a successful firing by detecting the heat generated
during ignition and relaying the information to a flare
detector in the electronic module. If no such information
is received, meaning that a flare was not successfully
fired, the module automatically fires another flare. If the
second flare also fails, a third flare is ejected. If the third
fails, the automatic sequence stops until one of the firing
switches is pressed again.
NO BREAK - WORK HARDER
With the successful firing of a flare, a 2.5 second delay
is imposed by the timer before another flare can be
fired. Readiness is signalled by the READY TO FIRE
light on the remote test panel coming on. With that,
the sequence may be repeated until all 30 flares have
been fired.
16-226
