RAD-HARDENED
VA41630
Radiation-Hardened Arm® Cortex®-M4
Provides the Highest Functional Density for Space-Based Applications.
The radiation-hardened VA41630 combines 100 MHz Arm Cortex-M4 performance, full mixed-signal peripherals, and integrated non-volatile FRAM into a single, high-reliability architecture.
Specifications
Built with >200 krad(Si) TID protection to virtually eliminate single-event latch-ups, it streamlines board design and minimizes SWaP for primary flight computers, satellite bus controllers, and 15+ year space missions
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• TID: > 200 krad(Si) with FRAM
• Soft Error Rate with EDAC & Scrub enabled: <1E-15 errors/bit/day
• SEL Immunity: >110 (MeVcm²) /mg @ 125°C
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• Core: 1.5 V ± 10%
• I/O: 3.3 V ± 10%
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• 64 KB on-chip Data SRAM
• 256 KB on-chip Program SRAM
• EDAC & Memory Scrubbing
• External SPI NVM
• External Bus Interface
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• 104 Configurable GPIO Pins
• 3xUART Interfaces
• 3xI2C Interfaces
• 3xSPI Interfaces
• 2xCAN 2.0 B
• Ethernet 10/100 MAC
• Full-Duplex Spacewire Interface
• 4-Ch DMA Controller
• 8-Ch ADC (12-bit, 600 ksps)
• 2-Ch DAC (12-bit)
• Integrated Temperature Sensor
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• 24 Configurable 32-bit Timers
• Input Capture, Output Compare, PWM, Counters, and Watchdog Timer
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-55° to 125°C
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• Plastic QFP 176 (20x20 mm)
• Plastic BGA 196 (12x12 mm)
• Ceramic QFP 176 (20x20 mm)
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• GEO and Deep Space Systems
• Single-Chip SmallSat On-Board Computers
• Scientific Instrument Control
• Motor & Actuator Control
• FPGA Reconfiguration & Management
• Satellite Bus Controllers
• Mechanism & Deployment Actuators
One Design
One Design, Two Radiation Profiles
RAD-TOLERANT
Meet the VA42630, the radiation-hardened twin to the VA41630
Prototype on the VA41630, then deploy the VA42630 in the same footprint for Medium Earth Orbit, Geosynchronous Earth Orbit, and deep space.
Support
Production qualified and shipping now. Supported by the PEB1 development board and software kit.
