At 149 mm outer diameter and 365 mm overall length, MAC400 combines its nominal thrust output with a compact engine package.
Propulsion selection should be assessed against the complete aircraft, including performance requirements, installation space, operating conditions and mission profile.
MAC400 can be considered for a new design, an existing platform or where an additional propulsion source is being evaluated.
MAC400 forms part of Milanion Group’s aerospace propulsion capability, with technical and commercial support covering integration, programme quantities, delivery and availability.
