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Case Study
IMMC: Integrated Mission Management Computer
Through expertise in designing SWaP-optimized systems, Curtiss-Wright designed the flight control computer with alternate mounting technique, which resulted in significant improvements in thermal performance, system reliability, and system performance.
06/25/2015
Case Study
Overcoming DAL-D Development Pitfalls with Modular Avionics COTS
This case study describes a crash-protected recorder designed by Curtiss-Wright to interface to a Data Management Unit (DMU) for a mid-range commercial airliner that had schedule challenges and changing requirements.
05/27/2015