The Mira 02Y-E camera — powered by the SCD Swift-EI sensor — is a significant advance in VIS-SWIR imaging, with a low SWaP-C architecture and advanced integrated features.
The VGA format camera uses a standard definition 640×512 format InGaAs detector with a 10μm pixel pitch, designed for SCD’s high volume semiconductor manufacturing process.
Mira features high-sensitivity and wide dynamic range. It provides real-time imaging with response across the Visible (VIS) through the SWIR waveband. Built-in Automatic Gain Control (AGC), image enhancement, and Non-Uniformity Correction (NUC) allow for seamless system integration and ease-of-use.
Data is provided through a MIPI interface. Control is accomplished via a serial port interface.
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.
Gas Turbine
Aircraft parts
