F20-THT

F20-THT PCIe/104 ATR Mission -GPU Computer
F20-THT PCIe/104 ATR Mission -GPU Computer

3/4 Short ATR

  • IP65 Air Borne Mission Computer 
  • 11th Gen Intel® Xeon® W-11865MRE (8C,16T) 4.7Ghz
  • Dual Redundant (A/B) MIL-STD-1553 Channels
  • 6 Channels of ARINC-429
  • Memory Up to DDR4-96GB  
  • NVMe 64GB Soldered On Board
  • NVIDIA MXM- RTX™ A4500, 16GB GDDR6 , 5888 CUDA 
  • Extreme Temperature -40~+60 Degree
  • MIL-461 18V~36V DC Input, Options for MIL-704/1275 10V~40V DC
  • MIL-STD 810 509 Salt Fog  Conformal Coating
  • MIL-STD 810 500.6 Low Pressure (50,000 ft) Altitude

 Intel Gold

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Introduction

ATR (Air Transport Rack) is a standard that specifies form fit and function of enclosures designed to protect the main internal system. This military enclosure must meet EMI / EMC requirements to prevent noise interference, provide lightning protection and be isolated from small particle contaminants. So, it can be deployed in unmanned aerial vehicles, fighters, and helicopters. To satisfy diverse conditions, ATR chassis are available in different sizes—1/2, 3/4 and Full ATR sizes.

 

F20-THT is an Air-Borne Mission GPU Computer that was designed to meet ATR 3/4 short size. F20-THT is built to withstand harsh environment by comply with MIL-STD 810 to sustain 75G shock and 10G vibration.

F20G

Block Diagram
F20G
ARINC 429

ARINC 429 is the worldwide standard for data transmission in aircraft electronics. It is adopted mostly for commercial aircraft and transport aircraft network protocol standard. Communications, guidance, altitude, altitude reference, flight management, and more are all needed to work together to accomplish a successful flight. The physical connection wires are twisted pairs carrying balanced differential signaling. 

The ARINC 429 unit of transmission is a fixed-length 32-bit frame, which the standard refers to as a 'word'. The bits within an ARINC 429 word are serially identified from Bit Number 1 to Bit Number or simply Bit 1 to Bit 32.

ARINC 429
MIL-STD-1553

MIL STD 1553 is US Military Department of Defence standard that was initially published in 1973. 

MIL STD 1553 is a differential serial bus. Also, it is a dual redundant data bus.  Each node is connected to each of the redundant buses.  Secondly, if one should fail, communications can still continue.

There are three types of operating nodes for 1553 Bus:

•A Bus Controller initiates all messages, traffic and commands the remote terminals to transmit/receive data.

•Remote Terminal interfaces the 1553 Bus and Sub System Bridge to other 1553 Buses.  It responds to the bus controller. 

•The Bus Monitor listens to messages and records them.

F20G

MIL-STD-810 & Full IP65 protection

F20-THT is designed to meet strict SWaP requirements and to withstand harsh environments, including extreme temperature, shock/vibration, sand/dust, and salt/fog. With ruggedized design and high functionality, the IP65 and MIL-STD resistance F20-THT is the ideal tactical vehicle on the battlefield.

F20G
F20G

System

High Power Processor

Xeon W-11865MRE (8 Cores/16 Threads, 24M Cache, up to 4.70 GHz), 45W

Memory type

Support up to DDR4-96GB

Chipset

RM590E

Storage

NVMe 64GB Soldered On Board

GPU

NVIDIA® MXM RTX™ A4500, 16GB GDDR6 memory, 5888 CUDA cores

ARINC 429 (optional)

6 Channels of ARINC-429

Channels: 4 RX/TX and 2 RX Only Channels. w/ mini-PCIe 

MIL -1553(optional)

1-2 INDEPENDENT,

DUAL REDUNDANT (A/B) MIL-STD-1553 CHANNELS w/ mini-PCIe card

(Alta-dt MPCIE2-1553)

TPM

TPM 2.0 (SLB9665)

BIOS

AMI SPI 256Mbit   

COM

2x RSRS232

USB

2x USB2.0

Ethernet

NIC1(optional)

NIC2(optional)

Intel I225 series (10/100/1000Mbps/2.5G)

2x 10G(SFP+)

2x 10G (RJ45)

Power Type

18V ~ 36V DC IN

Storage

1x 2.5” SATA SSD

Frame Grabber Type

HD-SDI or 3G-SDI, (2x CH)

Operating Temperature

-40°C to 60°C

Dimension

190.50(W) x 320.50(L2) x 269.88(H) mm 

FRONT I/O

 

X1

1x 10G LAN 

X2

1x 10G LAN

X3

1x 2.5G LAN

X4

2x USB + 1x DVI + 2x COM
X5 DC IN with D38999 connector
X6~X7 BNC
Valve 1x Waterproof valve

Environmental

 

MIL-STD-810 Test

Method 500.5, Procedures I and II (Altitude, Operation):

12,192M, (40,000 ft) for the initial cabin altitude (18.8Kpa or 2.73 Psia)

Method 500.5, Procedures III and IV (Altitude, Non-Operation):

15,240, (50,000 ft) for the initial cabin altitude (14.9Kpa or 2.16 Psia)

Method 501.5, Procedure I (Storage/High Temperature)

Method 501.5, Procedure II (Operation/High Temperature)

Method 502.5, Procedure I (Storage/Low Temperature)

Method 502.5, Procedure II (Operation/Low Temperature)

Method 503.5, Procedure I (Temperature shock)

Method 507.5, Procedure II (Temperature & Humidity)

Method 514.6, Vibration Category 24/Non-Operating (Category 20 & 24,Vibration)

Method 514.6, Vibration Category 20/Operating (Category 20 & 24,Vibration)

Method 516.6, Shock-Procedure V Non-Operating (Mechanical Shock)

Method 516.6, Shock-Procedure I Operating (Mechanical Shock)

Reliability

No Moving Parts; Passive Cooling.

Designed & Manufactured using ISO 9001 Certified Quality Program.

EMC

MIL-STD-461 :

CE102 basic curve, 10kHz - 30 MHz

RE102-4, (1.5 MHz) -30 MHz - 5 GHz

RS103, 200 MHz - 3.2 GHz, 50 V/m equal for all frequencies

EN 61000-4-2: Air discharge: 8 kV, Contact discharge: 6kV

EN 61000-4-3: 10V/m

EN 61000-4-4: Signal and DC-Net: 1 kV

EN 61000-4-5: Leads vs. ground potential 1kV, Signal und DC-Net: 0.5 kV

CE and FCC

Attachment Size
US20160231790A1 - PCI-104_0_0.pdf (1.14 MB) 1.14 MB