Mission management systems that meet ever-present size, weight, and power (SWaP) demands while providing the scalability and flexibility to handle all of the mission tasks today’s warfighter may encounter.

Whether looking for a modular, SFF LRU or a scalable VPX system designed to meet your program requirements, Curtiss-Wright computing systems are built rugged to perform optimally in the harshest deployed environments on land, in the air, or at sea.

COTS products and open-architecture solutions for mission computing, signal processing, graphics, communication fabrics, system and sensing I/O, and data storage.

This essential guide describes MOSA's significance for defense technology and the roles standards like SOSA, CMFF, CMOSS, VICTORY, GVA, and FACE play.

This white paper was presented at the 2021 NDIA Ground Vehicle Systems Engineering and Technology Symposium, Vehicle Electronics Architectures Technical Session, August 10-12, 2021.

As unmanned vehicles become more powerful and complex, their electronics payloads must adapt to match new mission objectives. This often forces aerospace and defense system integrators to push for reductions in size, weight, power, and cost (SWaP-C).

We examine the 2019 tri-services memo regarding MOSA and what open standards such as SOSA, FACE, and VICTORY mean for today’s military programs.

TCG HUNTR software installed on a Parvus DuraCOR 8043 mission computer, displayed on a GVDU mission display, provides operators with a rugged, small form factor solution that can be used on the battlefield with minimal training and almost no expertise.

When a large system integrator needed a SWaP optimized, rugged, network-attached storage system with NSA-approved encryption, a UAV contacted Curtiss-Wright for a trusted, proven solution.

Read about key similarities and differences between GVA and VICTORY and the benefits of using such frameworks in land vehicle upgrades and new builds.

A customer wished to move to the latest and greatest technology without having to change pinouts or cables on the aircraft.

The paper presents an open standards-based intra-vehicle network design approach applicable to multiple HBCT platforms using a common set of vehicle agnostic components, leveraging OpenVPX slot profiles and VICTORY Standards.