The Razorback-300 (RB-300) avionics single-board computer turbine engine monitoring system is an extremely compact and low-power, aerospace grade x86 compatible computer. Developed by Southwest Research Institute (SwRI), the RB-300 computes real-time engine parameters with simultaneous data capture. The RB-300 modernizes legacy aircraft systems while remaining compatible with previous generation support equipment.
- Form-fit function replacement for legacy avionics processor
- RS-422 and RS-232 interfaces
- Conduction cooled with wedge-locks
- Less than 4 W power consumption
- Environmental ruggedness:
- Temperature: -40 to 71°C operation
- Humidity: 95% non-condensing
- Military shock and vibration survivability
|Form Factor||High density. Small form factor
Measures just 4.87" H x 5.4" W
|CPU||ZF micro system-on-a-chip 486 compatible.
Processor running at 100 MHz. Integrated floating point.
Less than 1 W power consumption.
|Memory||Expandable 32 MB SDRAM system memory|
|MIL-STD-1553B||Dual-redundant MIL-STD-1553 interface capable of remote terminal, bus monitor, or bus controller|
|BIOS||ZF FailSafe Phoenix BIOS with headless console redirection|
|Non-Volatile Memory||Integrated 2 GB SST NANDrive™ upgradeable to 4 GB.
Extremely small form factor providing more than 100 million write cycles
10/100 Mbps Intel Pro 100 IEEE 802.3 compliant Ethernet controller
|Multi-I/O Port||2 x serial (1 x RS-232 and 1 x RS-232/422)
1 x FDD Port
1 x External 44 pin 2.5" drive header (master and slave)
1 x JTAG test and programming header
1 x ZTAG BIOS flash port
1 x MIL-STD-1553B
1 x 10/100 Mbps Ethernet
|Environment||EMI/EMC: MIL-STD-462A CE03 and RE02
Temperature variation: MIL-STD-810F 20°C/minute
Temperature and altitude: RTCA/DO-160D
Mechanical shock: MIL-STD-810
Temperature operation: -40 to 71°C
Altitude: 45,000 ft
|Ordering Information||Part Number 55578-0300-10|