Europrop International

TP400-D6

Turboprop In Production

Technical Specifications

Dry Weight
1.800 kg
Length
3,200 m
First Run
2005
In Service
2013

Europrop International TP400-D6

The TP400-D6 is the world's most powerful turboprop engine produced in the Western world, rated at an extraordinary 11,000 shaft horsepower (SHP) per engine. Developed by the Europrop International consortium — comprising MTU Aero Engines (Germany), Safran Aircraft Engines (France), Rolls-Royce (UK), and ITP Aero (Spain) — it was purpose-built to power the Airbus A400M Atlas strategic military transport. The TP400-D6 represents the pinnacle of Western turboprop technology and is one of the most complex propulsion systems ever certified.

Technical Specifications

ParameterValue
Shaft Horsepower11,000 SHP
Dry Weight1,800 kg (3,968 lb)
Length3.200 m (125.98 in)
First Run2005
Entry into Service2013
StatusIn Production

Three-Spool Architecture and Propeller System

The TP400-D6 employs a unique three-spool design — an arrangement more commonly associated with large civil turbofans (notably Rolls-Royce Trent engines) than with turboprops. The three spools rotate at independently optimized speeds: a low-pressure compressor spool, a high-pressure compressor spool, and a power turbine spool that drives the propeller gearbox. This configuration allows each compressor to operate at its aerodynamic optimum, maximizing overall thermal efficiency at very high power levels.

The propeller system is equally remarkable. Each TP400-D6 drives an 8-bladed Ratier-Figeac FH386 contra-rotating propeller (also referred to as a scimitar propeller system). On the A400M, the two inboard engines rotate their propellers in the opposite direction to the two outboard engines — a configuration chosen to minimize asymmetric torque effects and optimize airflow over the wing. The large-chord, swept composite blades absorb 11,000 SHP while operating at relatively low rotational speeds, reducing noise and improving efficiency.

Development Challenges

The TP400-D6 development program was technically ambitious and challenging. Integrating a three-spool core with a contra-rotating propeller system, across a four-nation industrial consortium, required solving complex control law problems to manage propeller interactions in all flight phases. Early flight testing revealed resonance and vibration challenges that required software and hardware modifications. These issues contributed to the A400M program's well-publicized delays, but by entry into service in 2013 the engine had been thoroughly validated.

The A400M's capability to carry heavy military cargo at turboprop fuel efficiency while landing on unprepared airstrips — a task jets cannot perform — depends entirely on the TP400-D6's exceptional power. With 11,000 SHP per engine and four engines total, the A400M's combined installed power approaches 44,000 SHP, enabling a maximum payload of 37 tonnes.