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|  MIL-E-7104D(WEP)
* 3.6.3.4.5 Ground Speed Indicator - The ground speed indicator shall indicate the muzzle
velocity at which rounds are to be ejected. The indicator shall be a digital veeder root type instru-
ment calibrated in knots of ground speed in one knot increments and shall have integral lighting.
* 3.6.3.4.6 Ground Speed Selector - A standard knob and crank shall be provided to operate
the muzzle velocity control circuits and ground speed indicator when the unit is in remote operation
3.6.3.4.7
Ready Indicator - An indicator light shall be provided which shall be lighted
when the equipment is ready in all respects for ejecting rounds with a release signal from the remote
control.
3.6.3.4.8
Release Switch - The release switch shall be a guarded push-button type switch.
Pressing the switch shall apply electrical power from the power switch shall apply to the firing valve.
* 3.6.3.4.9
Cover Box - The cover box shall be in accordance with 3.6.2.4.5.
*3.6.3.5
Electrical Connections - Connections to external circuits shall be provided by
an MS3102A-20-27P connector as follows:
Function
Pin Designation
A
Ground
28 V DC from local control
B
Ready indication
C
Spare
D
E
Muzzle Velocity Control
F
Load.
G
Bleed
H
Release
swing and feed
I
J
Muzzle velocity control
K
Auxiliary release input
L
Auxiliary release power output
M
Spare
N
Spare
*3.6.4
Air Reservoir TMK-60\A47U-1 - The air reservoir shall be a Type 30-58,
Class B. nonshatterable steel air reservoir in accordance with Specification MIL-R-8573. The
capacity of the air reservoir shall be 50 cubic inches minimum.
3.6.5
Magazine MAK-22A/A47U-1
*3.6.5.1
Function - The magazine shall be capable of stowing at least 20 rounds so that
they are accesible to the feed-mechanism of the launcher when the magazine is installed on the
launcher.
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