The HON1600 meets mission-critical parameters, including high-altitude capability up to 40,000 feet, rigorous G-level performance and the ability to reach manoeuvring targets. The USAF’s CCA programme is a multi-pronged initiative to test, develop and implement autonomous and manned-unmanned aircraft teaming concepts.
The propulsion system has been engineered to move “from model to metal” quickly, with many materials suitable for additive manufacturing and high-volume techniques such as metal injection moulding. This design approach aims to increase speed of production and strengthen supply chain resilience.
“We’ve designed this engine to meet the new generation of CCA and UAS platforms that require unprecedented performance to keep pace with mission demands. Our propulsion system is based on proven and tested technology in use today, plus the latest advancements in digital modeling and manufacturing, to enable a cost-effective and efficient solution for military operators,” said Dave Marinick, president, Engines and Power Systems, Honeywell Aerospace Technologies.
The engine’s flexible and scalable architecture supports turbojet or turbofan variants ranging from 800 to 1600 pound-force thrust, with scalability for additional requirements. Honeywell confirmed the core engine has already been demonstrated at rated thrust.
Using a systems engineering approach with digital modelling, Honeywell enables faster design, integration and more accurate evaluation at the air vehicle level. The HON1600 family is also designed to support long-term storage prior to deployment.
