Every

Vehicle.

Fleet.

Mission.

Powered and protected by Operational Intelligence.

Mission-First Mindset, Relentless Innovation, Data-Driven Precision

We're not just protecting today's systems that defend nations and power economies - we're building the digital operating system for tomorrow's fleets.

Active Electronically Scanned Array Radar

Azimuth: 45.0
Elevation: 10.0
Range: 50.0 km
Velocity: 300.0 mps
Description: AESA radar target track data

Common Integrated Processor

Scan Sector Start Angle: 40°
Scan Sector Width: 100°
Mode Code: Track While Scan
Azimuth: 32

Integrated Avionics

Roll: 5°
Pitch: 10°
Yaw: 45°
Altitude: 1000 meters
Track ID #: 161
Range: 47.3 nm
Bearing: 112°
Threat Level: High

Manifold Output

IFDL: Nominal
GPS/GNSS: Nominal
CIP: Nominal
IA: Failing
Ew: Nominal

GPS/GNSS Receiver

GPS Latitude: 64.665000° N
GPS Longitude: -147.102000° W
GPS Altitude: 5,401 ft
GPS Groundspeed: 551
GPS Track: 91.01°
GPS TOW = 345,601 s

Electronic Warfare

Threat Type: 1
Azimuth: 120.0°
Elevation: 15.0°
Range: 50 km
Description: Detected threat: SAM radar at 120.0° azimuth, 15.0° elevation, 50 km range

Intra Flight Data Links

Sender: Aircraft ID 23B
Track Index: 1112
Altitude: 28,000 ft
Velocity: 520 knots Friend IFF Flag: Set
Usage: Secure, LPI/LPD communication for F-22 intra-formation coordination
Stealth Considerations: Directional transmission minimizes detectability

Engine Control

Speed: 617.4 RPM
Coolant Temp: 60 °C
Fuel Pressure: 61.0 kPa
Fuel Rate: 1566.6 L/h
Oil Pressure: 360 kPa

Common Launcher Control Unit

System Mode: Standby
Azimuth: 45.25 °
Elevation: 2990 mils
Slew Rate: 98 mils ps
Pod Selected: A
Tube Selected: 3
Power Main Bus: 27.9 volts
Power Battery: 25.1 volts
Power Current Draw: 12.4 amps
Internal Temp: 32.5 °C
Hydraulic Pressure: 2850 PSI
Vibration Level: 0.12 g

Manifold Output

GPS/GNSS: Nominal
FCS: Nominal
WCU: Nominal
EC: Failing
PSU:
CLCU: Nominal

Power Switching Unit

Voltage: 28.2 volts
Current: 23.4 amps
Temp: 38 °C
Channel 1 FCS CPU: ON
Channel 2 IMU: ON
Channel 3 GPS: ON
Channel 4 Actuator A: ON
Channel 5 Actuator B : ON
Channel 6 Radio: ON
Channel 7 Ethernet Switch: ON
Faults: “OC WARN - CH5 ActB, Duration 50ms, Cleared"

Fire Control System

Target Latitude: 39.99872°
Target Longitude: -77.04521°
Target Elevation: 254.1 m
Munition Code: M31A1
Launcher Azimuth: 124.60°

Weapon Control Unit

System Mode: Armed
Pod Temperature: 25.0 °C
Fault
Flags: No Faults
Status: Ready

GPS/GNSS Receiver

Latitude: 38.8897
Longitude: -77.0091
Altitude: 120.5 m
Ground Speed: 215.3 mps
ing: 84.2 °
Time: Thursday 09:54 UTC
Satellites Tracked: 11
Signal Strength: 81 dB

GPS/GNSS Receiver

Latitude: 36.818723
Longitude: -76.2927967
Altitude: 12.3 meters
Satellites Visible: 12
Signal Strength: 81 dB
Speed: 0.2 knots
Course: 18.0 °
Fix Quality: RTK

Combat Information Unit

Weapon System: Mk 41 VLS
Target Track #: 04512
Engagement Mode: AUTO
Assigned Missile: SM-2 Block IIIC
Launch Bearing: 097 °
Predicted TOF: 88 sec
Status: READY_TO_FIRE
Timestamp: 2025-08-14T13:42:15Z

Radar Signal Processors

Frame ID: 0001
PRF: 3200 Hz
Pulse Width: 4.5 µs
Antenna Face: Port
Beam Position: 102.35°, 2.15°
Sample Count: 4096
Data (first 16 I/Q pairs):
I: +124, Q: -55
I: +120, Q: -49
I: +117, Q: -42
I: +115, Q: -40
I: +113, Q: -37
Timestamp: 2025-08-15T14:02:17.128Z

Manifold Output

PCU: Nominal
RSP: Nominal
CIU: Nominal
IPACM: Nominal
GCS: Nominal
GPS/GNSS: Spoofing

Gun Computer System

Target ID: TGT-073
Target Type: SURFACE
Bearing: 142.5° (relative)
Range: 12,400 yds
Target Speed: 18 kts
Target Course: 275°
Lead Angle: +2.1°
Elevation Angle: +5.6°
Time of Flight: 21.3 sec
Number of Rounds: 3
Fuze Mode: VT (Variable Time)
Status: READY_TO_FIRE
Timestamp: 2025-08-14T13:50:12Z

Integrated Power & Auxiliary Control Modules

Bus Voltage: 250.0 V
Frequency: 30.6 Hz
Real Power: 150.0 kW
Breaker Main: CLOSED
Bus Tie A: CLOSED
Alarm Word A: none
Alarm Word B: Overtemp Warning

Propulsion Control Units

Turbine RPM: 3600 rpm
T5 Temperature: 890.0 °C
Lube Oil Pressure: 145.0 psi
Fuel Flow: 1200 pph
Vibration: 0.120 in/s
Gearbox Temp: 82.0 °C
Shaft Torque: 18000 ft-lb
Status Bits: RUN(0)

GPS/GNSS ReceiveR

Status: Warning Spoofing Detected
Latitude: 40.12345N
Longitude: -76.98765W
Altitude: 1,001
Satellites Visible: 8
Signal Strength: 81 dB

Positive Train Control

Time: 12:00:01.245
From: Loco 4821
To: Dispatch Tower 23
Msg Type: Train Status Update
GPS: 40.12345N, -76.98765W
Speed: 43 mph
Authority: Milepost 122.3 to 145.0
Brake Status: Released

Brake Control

Cylinder Pressure: 90 PSI
Pipe Pressure: 144 PSI
Application Status: Apply
Fault Code Status: No Fault
Cylinder Pressure: 96 PSI
Pipe Pressure: 146 PSI

Engine Control

Speed: 617.4 RPM
Coolant Temp: 60 °C
Fuel Pressure: 61.0 kPa
Fuel Rate: 1566.6 L/h
Oil Pressure: 360 kPa

Traction Control

Traction Motor Current: 8000 Amps
Axle Speed Sensor: 122 RPM
Wheel Slip Event: No Slip
Tractive Effort: 20,000 lbf
Traction Motor Current: 8005 Amps
Axle Speed Sensor: 121 RPM

Propulsion System

Torque: 8512 Nm

Speed: 5032 RPM

Current: 68 Amps
Voltage: 604 Volts

Manifold Output

PTC: Compromised
TC: Nominal
PS: Nominal
GPS/GNSS: Nominal
BC: Nominal
EC: Nominal

01 /

Active Electronically Scanned Array Radar

S5 Formatted Data

Azimuth: 45.0
Elevation: 10.0
Range: 50.0 km
Velocity: 300.0 mps
Description: AESA radar target track data

Title
0x08FC  0x0005  0x4601  0x17B0  0x321A  0xC16B  0x8E09  0x5460  0x0BB8  0xFE0C  0x0A03  0xA500

Built for the field and tested in the most demanding environments, our technology equips operations, maintenance, and cybersecurity teams with the infrastructure and analytics to detect threats, anticipate failures, and respond with confidence.

How it works.

00 /05

  The Shift5 platform collects, processes, and analyzes data from your platform to deliver full visibility into cyber threats and maintenance issues – from the edge to the operations center.

1
Data Capture
2
Threat Detection
3
Post-Mission Investigation
4
Fleet-Wide View 
5
Ongoing Updates 
Data Capture

Shift5 hardware connects directly into a platform’s serial bus networks to capture mission data during live operations. 

Threat Detection

Near real-time anomaly detection alerts operators and ground crews to emerging cyber threats or maintenance risks for immediate awareness and action.

Post-Mission Investigation

Post-mission data access equips cyber and maintenance groups with insights for forensic investigation to optimize future platform performance.

Fleet-Wide View 

A unified dashboard provides commanders with full visibility into the status of their fleet to inform operational readiness. 

Ongoing Updates 

Shift5 software is continually updated with new detections and capabilities to provide added value over time. 

Manifold 4

Manifold 10

Shift5 BIC

Manifold 4 is a small and lightweight data collection device that easily slots into all air, ground, and maritime platforms. The Manifold 4 ingests data from up to 4 different serial bus protocols simultaneously with at-rest encryption for bolstered security. Additional capabilities include near real-time alert streaming for platform operators and ground control stations and a ruggedized design to survive harsh environmental conditions. Less

Manifold 4 is a small and lightweight data collection device that easily slots into all air, ground, and maritime platforms. The Manifold 4 ingests... More

Manifold 10 is a variant of the Manifold 4 designed for commercial aviation to manage higher data capacity. The Manifold 10 ingests data for up to 110 channels for a variety of serial bus protocols, including ARINC 429, ARINC 717, ARINC 664, and gigabit ethernet. Less

Manifold 10 is a variant of the Manifold 4 designed for commercial aviation to manage higher data capacity. The Manifold 10 ingests data for up to... More

The Bus Interface Card (BIC) inserts into Manifold 4 and Manifold 10 devices to enable full data capture across all serial bus protocols. The BIC is custom designed to deliver full visibility into serial bus activity down to the physical layer to uncover anomalies in bus traffic and indicators of hardwire degradation. The BIC supports data capture on up to 12 channels for a variety of serial bus protocols, including CAN, MIL-STD-1553, and ARINC 429. Less

The Bus Interface Card (BIC) inserts into Manifold 4 and Manifold 10 devices to enable full data capture across all serial bus protocols. The BIC is... More

Manifold 4 is a small and lightweight data collection device that easily slots into all air, ground, and maritime platforms. The Manifold 4 ingests data from up to 4 different serial bus protocols simultaneously with at-rest encryption for bolstered security. Additional capabilities include near real-time alert streaming for platform operators and ground control stations and a ruggedized design to survive harsh environmental conditions.

Manifold 10 is a variant of the Manifold 4 designed for commercial aviation to manage higher data capacity. The Manifold 10 ingests data for up to 110 channels for a variety of serial bus protocols, including ARINC 429, ARINC 717, ARINC 664, and gigabit ethernet.

The Bus Interface Card (BIC) inserts into Manifold 4 and Manifold 10 devices to enable full data capture across all serial bus protocols. The BIC is custom designed to deliver full visibility into serial bus activity down to the physical layer to uncover anomalies in bus traffic and indicators of hardwire degradation. The BIC supports data capture on up to 12 channels for a variety of serial bus protocols, including CAN, MIL-STD-1553, and ARINC 429.

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Get in touch to learn more.

Phone

+1 703 810 3320

General Inquiries

info@shift5.io
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