The GE-Rolls-Royce Fighter Engine Team recently completed
a high-altitude afterburner testing program of the engine,
proposed as an alternative to the F135 currently flying on
the F35s prototypes. These tests were performed at the US
Air Force Arnold Engineering Development Center in Tennessee,
with engines configured with Conventional Takeoff and Landing
(CTOL) and Short Takeoff Vertical Landing (STOVL) common exhaust
systems. The engine configuration included a production-size
fan and functional augmentor allowing several run periods
to full afterburner operation. The two engines being tested
were produced during the pre-System Development and Demonstration
(SDD) phase. CTOL test objectives were successfully accomplished
in mid-March 08. STOVL testing continue for several weeks
to come. Representing the latest configuration, the original
powerplants have been updated with new fan, augmentor and
controls technology designed during the SDD process.
The pre-SDD engines have totaled more than 600 hours of test
time, contributing significantly to risk reduction in the
program. The first full SDD engine is scheduled to begin testing
by early 2009, with first flight in the F-35 to follow in
2010. The SDD phase is scheduled to run through 2013; the
first production F136 engines are scheduled to be delivered
in 2012 for the F-35 Lightning II aircraft. This occurs during
the fourth lot of F-35 aircraft production, which is very
early in the overall aircraft production program. The F136
will be fully interchangeable for the F-35. The F136 was the
first F-35 engine to offer a single engine configuration for
all three versions of the aircraft: STOVL for the U.S. Marine
Corps and U.K. Royal Navy, Conventional Takeoff and Landing
(CTOL) for the U.S. Air Force, and the Carrier Variant (CV)
for the U.S. Navy.
The two team partners share the work on the F136 with GE
- Aviation, responsible for 60 percent of the F136 program,
developing the core compressor and coupled high-pressure/low-pressure
turbine system components, controls and accessories, and the
augmentor. Rolls-Royce, with 40 percent of the F136 program,
is responsible for the front fan, combustor, stages 2 and
3 of the low-pressure turbine, and gearboxes. International
participant countries are also contributing to the F136 through
involvement in engine development and component manufacturing.