8 Fields on FCU
1) Power
2) Miscellaneous
3) Mode
4) Gun
5) Sight
6) Grenade
7) Battle Override
8) Menu
Elevation Speed
MIN: .15 mils/sec
MAX: 60 degrees/sec
Traverse Speed
MIN: .15 mils/sec
MAX: 80 degrees/sec
Locks
1) Stow/Azimuth Transport and Travel Lock (SATTL)
2) Stow Elevation Transport Lock (SETL)
3) Azimuth Release Mechanism/Lock System (ARMLS)
4) Elevation Manual Mode Release Lever (EMMRL)
Elevation/Depression Zone
Front: -10 to 60 degrees
Rear: 60 to 0 degrees
Smoke Grenades
M6 SGLs: Each with 4 smoke grenade tubes.
Total tubes: 16
Detonating range: 30ft.
Caliber: 66mm
Obscuration cloud: 6 to 7m high
Covering arc: 30 degrees per launcher, 15.5 degrees per tube, 14.5 degrees spread between launchers
Fire Controller Software
Main computer/ Manager of the RWS.
All data is accumulated or contained in the FCS, including the Soldier Machine Interface, except the operation of the Control Grip.
Servo Controller
Ballistic Solutions
Calculated using ammo type, range to target, and the pitch and roll of the sight axis relative to the HP (measured by the inclinometer).
Ballistic tables are used to find the TE and drift angles, allowing for automatic ballistic control solution resulting in enhanced first round hit capability.
Sensor Calibration
Used to map the servo position decoders with the absolute sensors for azimuth and elevation.
Should be done when the FCU, Main Frame Assembly, or the RSSA has been replaced.
Ammunition Load
.50 CAL: 20 Cans
MK19: 10 Cans
Smoke Grenades: 32
W3 Cable
Delivers video signals from the sensors to the FCU and power to the WS.
W2 Cable
Delivers data and video/signal feedback from the FCU to the WS.
W1 Cable
Connects CG to FCU and delivers power and signal/feedback.
Pedestal Hinge Mechanism
Required to hinge the RWS forward for transport purposes. Allows the RWS to clear the height restriction for transport in a C-130 (106in.). Can also be used for rail and highway transport.
Sensor Controller
Handles communication between the FCU and the sensors as well as controlling the cocking actuator.
Located in the SSA
Controls:
- STORM LRF
- VIM
- TIM
- Low Ammo Sensor
- Inclinometer
TIM WFOV/NFOV
WFOV: 10 degrees used for target identification
WFOV with 2x Digital Zoom: 5 degrees used for target identification
NFOV: 3.3-degree target ID out to 1,500m
NFOV with 2x digital zoom 1.7-degree target ID out to 2,000m
STORM LRF (Power and Data)
P-4: Power
P-5: Data. Enables remote operations from the CG
Range Button (SCALE)
Scale is from 100m to 2,200m. Default is 700m.
Soldier Machine Interface
Operated by the Fire Controller Software
5 STORM LRF Lasers
1) Laser Range Finder
2) Visible (VIS) Aim Laser (VL or VH)
3) Infrared (IR) Aim Laser (AL or AH)
4) Adjustable Infrared Illuminator
5) Tactical Engagement Simulation System/Multiple Integrated Laser Engagement (TESS/MILES) Laser
VIM Discrete Steps
(Degrees)
1.7
3.3
5
10
25
47
Hatch Interrupt Unit (HIU)
Supplies the RWS with a vehicle ID.
Tubular Cocking Actuator
Used for automative cocking the weapon. Consists of an electric motor with a moving cocking rod with cocking bracket and forces the cocking bracket forward.
Driven by the FCU through the W4 cable/J3 connector.