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Military-Ruggedized


    • It is aligned with the SOSA™ (Sensor Open Systems Architecture) standard.
    • The processor used is the Intel® Core™ i7-1186GRE with integrated PCH-LP (Tiger Lake) with 4 cores and 12M Smart Cache and it runs at speeds up to 2.8 GHz.
    • The 68INT6 offers off-the-shelf solutions, which means it is readily available for deployment.
    • It enables the acceleration of SWaP-optimized (Size, Weight, and Power) systems in air, land, and sea applications.

     

  • The rugged PCC01 Mission Computer from Core Systems is a rugged custom-built sealed fanless tactical computer build for the military.

    • Extended temperature design with a range of -40C to +85C.
    • Tested for MIL-S-901D Shock, MIL-STD-167-1 Vibration, MIL-STD-810G Shock & Vibration, MIL-STD-810F Humidity, and MIL-STD-461E/F EMC.
    • Includes a 500GB solid-state drive which is installed in a removable carrier.
    • Application-Specific
    • Military-Grade Design

     

  • The AR8 is a small, rugged, and SWaP-optimized tactical mission computer with the latest Intel Gen CPU.

    • Fully conduction-cooled
    • Small Form Factor (SFF)
    • Utilizes proprietary thermal transfer technology to cool the system without the use of moving parts
    • Completely sealed chassis built to survive extreme temperature, shock, and vibration

     

  • The RPS317 laptop has a rugged MIL-Spec 16-Core portable server with 2x the CPU performance of the previous 16-Core RPS217 in a lighter chassis.

    • 17.3” HD LCD
    • Upgraded 16-Core Xeon CPU
    • 512GB RAM with dual SSD drives.
    • Engineered for high shock/vibration and wide temperature.
    • The onboard Intel Xeon 16-Core processor provides true server-class performance in a compact rugged portable form factor.
    • 2 x Redundant MIL-STD-1553 Channels
    • 8 x ARINC-429/575 Tx/Rx Channels
    • 8 x RS-232/422/485 Sync/Async Serial Channels
    • 28 VDC Input PSU with 50 ms holdup option

    • 2 x Redundant MIL-STD-1553 Channels
    • 8 x ARINC-429/575 Tx/Rx Channels
    • 8 x RS-232/422/485 Sync/Async Serial Channels
    • 28 VDC Input PSU with 50 ms holdup option

     

  • with 10 GB Fiber Optic & 1 GB Copper Ethernet Switch

    • Preconfigured embedded I/O Functions: 24-CH Discrete I/O, 8-CH ARINC 429/575, 4-CH CANBus (programmable for CAN 2.0A/B, ARINC 825 or CAN FD protocol) and 2-CH MIL-STD-1553
    • Ethernet switch module that offers four (4) 10GBase-SR multimode fiber optic ports and sixteen (16) 10/100/1000Base-T Ethernet ports
    • Supports One NAI smart I/O function module
    • Minimized SWaP Footprint
    • Xilinx UltraScale+ SoC with Dual/Quad Core ARM Cortex®-A53 processors
    • 28 VDC Input Power Supply (50+ ms Hold-up Option)
    • DO-178C & DO-254 DAL A (Contact Factory)
    • Cybersecurity & Anti-Tamper (Contact Factory)

     

  • 6x 3U OpenVPX MOSA Remote Interface Unit

    • 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
    • 8 x RS-232/422/485 Serial Channels (SC3)
    • 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
    • 8 x Programmable RTD or Thermocouple measurement (TR1)
    • 16 x ±100 VDC A/D Channels (ADF)
    • 8 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
    • 2 x AC Reference Excitation (AC2)
    • 4 x Strain Gage Measurement (SG1)
    • 8 x Variable Reluctance/Pulse Counter Measurement Channels (VR1)
    • 16 x 10/100/100 Base-T Ethernet Switch (ES2)
    • 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
    • 28 VDC MIL-STD-704 Aircraft Electrical Power Characteristics with at least 50 ms holdup.
    • MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

     

  • 4x 3U OpenVPX MOSA Remote Interface Unit

    • 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
    • 8 x RS-232/422/485 Serial Channels (SC3)
    • 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
    • 8 x Programmable RTD or Thermocouple measurement (TR1)
    • 8 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
    • 2 x AC Reference Excitation (AC2)
    • 4 x Strain Gage Measurement (SG1)
    • 8 x Variable Reluctance/Pulse Counter Measurement Channels (VR1)
    • 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
    • 28 VDC MIL-STD-704 Aircraft Electrical Power Characteristics with at least 50 ms holdup.
    • MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

     

  • 6x 3U OpenVPX MOSA Mission Computer

    • 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
    • 8 x RS-232/422/485 Serial Channels (SC3)
    • 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
    • 4 x MIL-STD-1553/1760 (2 x FTJ)
    • 4 x Non-Latching Relay (RY1)
    • 24 x Enhanced Programmable Discrete I/O Channels (DT4)
    • 16 x ±100 VDC A/D Channels (ADF)
    • 12 x ±10 VDC or ±25 mA D/A Outputs (DA1)
    • 12 x ±1.25 to ±10.0 A/D Channels (AD1)
    • 12 x ±100V A/D Channels (AD2)
    • 16 x ±1.25 to ±10.0 VDC A/D Channels (AD4)
    • 16 x 10/100/100 Base-T Ethernet Switch (ES2)
    • 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
    • 28 VDC Input PSU per VITA 62 (VPX68) Optional 50 ms holdup.
    • MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

     

  • 4x 3U OpenVPX MOSA Mission Computer

    • 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
    • 8 x RS-232/422/485 Serial Channels (SC3)
    • 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
    • 24 x Enhanced Programmable Discrete I/O Channels (DT4)
    • 16 x ±100 VDC A/D Channels (ADF)
    • 12 x ±10 VDC or ±25 mA D/A Outputs (DA1)
    • 16 x 10/100/100 Base-T Ethernet Switch (ES2)
    • 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
    • 28 VDC Input PSU per VITA 62 (VPX68) with Optional 50 ms holdup.
    • MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

     

  • 2x 3U OpenVPX MOSA Mission Computer

    • 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
    • 8 x RS-232/422/485 Serial Channels (SC3)
    • 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
    • 24 x Enhanced Programmable Discrete I/O Channels (DT4)
    • 16 x ±100 VDC A/D Channels (ADF)
    • 12 x ±10 VDC or ±25 mA D/A Outputs (DA1)
    • 28 VDC Input PSU per VITA 62 (VPX68). Optional 50 ms holdup.
    • MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

     

  • 2x 3U OpenVPX MOSA Flight Control Computer

    • 8 x ARINC-429 Tx/Rx & 12 Programmable Discrete IO (CM2)
    • 16 x ±100 VDC A/D Channels (ADF)
    • 8 x Programmable RS-232/422/485 Serial Channels (SC3)
    • 2 x AC Excitation References (AC2)
    • 4 x LVDT Measurement Channels (LD2)
    • 4 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
    • 28 VDC Input PSU per VITA 62 (VPX68) with at least 50 ms holdup
    • MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.