Military Avionics Sensor Interface System

Aerospace and Defense Application

Description

Comprehensive sensor interface solution for military avionics applications featuring multi-protocol communication, signal conditioning, and extreme temperature operation for reliable performance in harsh aerospace environments.

Core Advantages

Multi-protocol support in single unit reduces system complexity
Extreme temperature range (-55°C to +175°C) for engine bay deployment
Comprehensive sensor conditioning eliminates external circuitry
Military-grade EMI immunity per MIL-STD-461
Redundant communication paths ensure system reliability

Recommended Bill of Materials (BOM)

Item Part Number Description Quantity Datasheet
1 MXD2420 24-Bit Sigma-Delta ADC 8 📄 Download
2 MXSC8808 8-Channel Signal Conditioner 4 📄 Download
3 MXD5303 Triple Output DC-DC Converter 4 📄 Download
4 MXRS48530 Isolated RS-485 Transceiver 4 📄 Download
5 MXCAN1050 Isolated CAN Transceiver 2 📄 Download
6 MX1553 MIL-STD-1553 Transceiver 2 📄 Download

Applications

Military Aircraft
Helicopter Systems
UAV Platforms
Engine Monitoring
Flight Control Systems

Technical Specifications

Analog Inputs
32 single-ended or 16 differential
A D C Resolution
24-bit
Sampling Rate
Up to 4.8 kSPS per channel
Input Range
±2.5V, ±5V, ±10V, 4-20mA
Sensor Excitation
Programmable 5V, 10V, 24V
Communication Protocols
MIL-STD-1553, ARINC 429, CAN 2.0B, RS-485
Isolation
2500Vrms channel-to-channel and channel-to-bus
Power Input
28VDC (16-32V range)
Power Consumption
<5W typical
Operating Temperature
-55°C to +175°C
Vibration
MIL-STD-810G, Category 14
Shock
MIL-STD-810G, Procedure I
E M I
MIL-STD-461G, CE102, RE102, RS103

Customer Success Stories

Military Aircraft OEM

|

Challenge

A military aircraft manufacturer needed a sensor interface system for their next-generation tactical aircraft engine monitoring. The system needed to operate in the extreme temperature environment of the engine compartment (up to 175°C), interface with 24 diverse sensors, and communicate over both MIL-STD-1553 and CAN bus for redundancy. The solution also needed to meet stringent military qualification requirements.

Solution

Deployed the Mxtronics military avionics sensor interface solution with 32-channel acquisition capability using MXD2420 sigma-delta ADCs and MXSC8808 signal conditioners. The multi-protocol architecture provided simultaneous MIL-STD-1553 and CAN bus interfaces. All components were selected for 175°C operation and full military qualification.

Results

"The Mxtronics solution met every requirement including the extreme temperature operation we needed for the engine bay. The multi-protocol capability simplified our system architecture and improved reliability through redundancy."

Rotorcraft Manufacturer

|

Challenge

Needed comprehensive sensor interface for helicopter health and usage monitoring system (HUMS) with vibration analysis capability.

Solution

Implemented 32-channel Mxtronics interface with high-speed sampling for vibration analysis and health monitoring.

Results

"The Mxtronics solution provides the reliability and performance we need for critical rotorcraft applications."

FAE Expert Insights

S

Senior FAE

Applications Engineer

10+ years

Professional Insights

For military avionics applications, the most critical design consideration is often the thermal management in high-temperature zones like engine compartments. The MXD2420 sigma-delta ADCs maintain excellent performance even at 175°C, but I always recommend keeping them away from direct engine mounting if possible. For the communication interfaces, implementing both MIL-STD-1553 and CAN provides the redundancy required for flight-critical systems. When laying out the PCB, pay special attention to the isolation barriers - the 2500Vrms rating requires careful spacing and slotting. I've seen several designs fail qualification due to insufficient creepage distances. For sensor excitation, use the programmable features of the MXSC8808 to optimize for each sensor type rather than using a one-size-fits-all approach. Thermal modeling and proper PCB layout are essential for success in these harsh environments.

Key Takeaways

  • Implement thermal modeling early in the design
  • Keep ADCs away from direct engine mounting when possible
  • Use separate ground planes for analog and digital sections
  • Verify creepage and clearance distances against MIL-STD-275

Decision Framework

Military Avionics Sensor Interface Decision Framework
Steps:
  1. Assess thermal environment and identify hot spots
  2. Select components rated for maximum temperature with margin
  3. Design PCB with proper isolation and spacing
  4. Implement redundant communication paths
  5. Optimize sensor excitation for each sensor type

Ready to Implement This Solution?

Contact our FAE team for design support and quotes

Contact Us Now

Frequently Asked Questions

What military standards does this solution comply with?

The military avionics sensor interface solution complies with multiple military standards: MIL-STD-810G for environmental testing (vibration, shock, temperature, humidity), MIL-STD-461G for electromagnetic interference, MIL-STD-1553B for the 1553 bus interface, MIL-STD-704F for aircraft electric power characteristics, and MIL-STD-883 for component screening. Full test reports and certificates of conformance are available.

Verify specific military standard requirements for your program. Contact us for detailed compliance documentation.

Can the solution be modified to add ARINC 664 (AFDX) support?

Yes, ARINC 664 (AFDX) support can be added to the solution by incorporating additional interface components. Mxtronics offers AFDX interface ICs that can be integrated into the architecture. The modular design allows protocol cards to be added or removed based on application requirements. Contact our applications engineering team for custom protocol configurations including AFDX, Ethernet, and other modern avionics interfaces.

Define your protocol requirements early in the design cycle. Consider future protocol migration needs when selecting the base configuration.

What is the qualification testing that has been performed?

The solution has undergone comprehensive qualification testing including: High Temperature Operating Life (HTOL) at 175°C for 1000 hours, Temperature Cycling from -55°C to +175°C for 500 cycles, Mechanical Shock per MIL-STD-810G Method 516.8, Vibration per MIL-STD-810G Method 514.7, Salt Fog per MIL-STD-810G Method 509.7, and EMI/EMC per MIL-STD-461G. All testing was performed by certified laboratories with full documentation.

Review qualification test reports for your specific application requirements. Additional testing can be performed if required by your program.

How many sensors can the system interface with?

The standard configuration supports 32 single-ended or 16 differential analog inputs. Each input can be configured for various sensor types including voltage output, current loop (4-20mA), thermocouples, and RTDs. The modular architecture allows expansion to 64 channels or more by adding additional acquisition modules. Digital sensor interfaces via MIL-STD-1553, CAN, or RS-485 can support hundreds of additional sensors.

Calculate total sensor count including analog and digital interfaces. Contact FAE for expanded channel configurations.

What sensor excitation options are available?

The MXSC8808 signal conditioners provide programmable excitation sources: 5V, 10V, or 24V for bridge sensors and transmitters. Current excitation is available for RTDs and other resistive sensors. All excitation sources are current-limited for protection and can be enabled/disabled under software control for power management. The excitation voltage is monitored for fault detection.

Verify sensor excitation requirements. Select appropriate excitation voltage and type for your sensors.