The MTU Hybrid Propulsion Pack combines various technologies for efficient energy management, ensuring minimum emissions and operational reliability for naval and commercial applications.
The AE 3007 turbofan engine, derived from the AE 1007C-Liberty engine, provides thrust in the 8,000lbf class. It features a high bypass ratio, a 14-stage compressor, and an effusion-cooled annular combustor, offering reliable performance.
The BR710 engine offers fuel efficiency and the capability to operate from hot/high airports, supporting long missions or long-distance flights. It powers VIP and Head-of-State missions on Bombardier and Gulfstream platforms.
The M250 turboprop is known for its compact size, high power-to-weight ratio, and adaptability to various aircraft types. It operates on all certified fuels and provides smooth, reliable performance.
The TP400-D6 incorporates proven commercial and military gas turbine technologies to deliver reliable propulsion for applications like the Airbus A400M military transport aircraft.
The T56 turboprop is renowned for its robust design and operational reliability in military and civil aviation, powering platforms like the C-130 Hercules and P-3 Orion.
The AE 2100 engine supports aircraft like the C-130J Hercules and C-27J Spartan, known for its modular design and high part commonality, enhancing operational efficiency and reducing maintenance costs.
With more than 31,000 units delivered and over 250 million flight hours, the M250 turboshaft is highly reliable, powering a range of rotary-wing aircraft.
The MTR390 is a collaborative turboshaft engine developed by Rolls-Royce, MTU, and Safran Helicopter Engines, offering reliable performance for modern rotary-wing platforms.
Proven during the RAH-66 Comanche program, the CTS800 engine has become a leading choice for production applications, offering reliable, high-performance turboshaft capabilities.
The AE 1107C is a unique 7,000 shp power plant with improved ‘hot and high’ performance. It features a two-shaft axial design with a 14-stage compressor, dual FADECs, and a self-contained oil system, enabling vertical operation.
The Adour twin-spool turbofan engine delivers thrust in the range of 5,000 to 8,000 lb and is known for its reliability and cost-efficiency. The Adour Mk 951 features Full Authority Digital Engine Control (FADEC) for enhanced control.
The Pegasus 11-61 variant provides up to 15% more thrust at high temperatures and features reduced maintenance requirements. It powers radar-equipped Harrier II+ with STOVL capabilities, still in service with the US Marine Corps.
The RB199 engine powers all variants of the Tornado combat aircraft and has accumulated over 7 million flight hours. It offers a compact design with a high thrust-to-weight ratio and low fuel consumption.
The Rolls-Royce LiftSystem® is the sole vertical lift technology for the F-35B Lightning II. It offers responsive and precise STOVL capability through components like the LiftFan®, Driveshaft, and 3 Bearing Swivel Module (3BSM).
