WRIGHT-PATTERSON AIR FORCE BASE, Ohio (AFNS) –
Members of the Air Force Research Laboratory and Lockheed Martin's famed 'Skunk Works' launched a new era of aircraft manufacturing technology and performance with the successful initial demonstration flight of the Advanced Composite Cargo Aircraft June 2 at Air Force Plant 42 in Palmdale, Calif.
The ACCA is a modified Dornier 328J aircraft with the fuselage located to the rear of the crew station and the vertical tail removed and replaced with completely new structural designs made of advanced composite materials fabricated using lower pressure and temperature.
The ACCA fuselage is wider and stronger to accommodate military standard 463L pallets and features a cargo door and cargo ramp. The vertical tail features integrally stiffened skin. Despite its larger size, the materials and processes used for the fuselage reduced the number of parts by an order of magnitude relative to the original metallic design, approximately 300 versus 3,000, and drastically reduced the number of mechanical fasteners, about 4,000 vs. 30,000, program officials said.
Lockheed Martin officials said the ACCA took-off to the east from Air Force Plant 42 at 6:55 a.m. Pacific Time. The aircraft then banked west and climbed to an altitude of approximately 10,000 feet where the two-pilot crew took the vehicle through a series of airspeed, stability and control tests. Officials said the tests are important to understand how the composite cargo aircraft performs at varying speeds, attitudes and altitudes. This data will be used as a baseline for future tests.
Duration for the first flight was about 87 minutes.
Barth Shenk, an ACCA program manager from AFRL's Air Vehicles Directorate at Wright-Patterson AFB, said the ACCA isn't designed to be a prototype for a small airlifter or any other aircraft. It is a proof of concept technology demonstrator for composite manufacturing processes in a full-scale, certified aircraft. In an effort to demonstrate and test the technologies while keeping costs down and on schedule, the small team of Air Force and Lockheed Martin engineers elected to modify the high-wing Dornier jet, mating its existing engines, wing, landing gear and avionics systems to the new composite structure. The modified fuselage has enlarged rear cargo doors and can accommodate two standard size military pallets.
The new composite structure is manufactured without complex tooling and the bonding process yields a 90 percent reduction of structural components and fasteners, said Frank Mauro, the vice president of advanced system development for Lockheed Martin.
"Historically aircraft cost has been generally determined by the size and weight of the vehicle. With ACCA, we are proving that while size does matter, it isn't the be-all, end-all determination of aircraft cost," Mr. Mauro said.
Lacking traditional fasteners like rivets, the composite structure is inherently aerodynamic. Mr. Shenk said he believes composite structures will address many of the corrosion and aging issues associated with all-metal aircraft, reducing airframe lifetime maintenance. Lighter weight of composite materials can also contribute to increased cargo capacity, aircraft performance and lower operating costs. The real game changer, however, is the maturation of manufacturing processes, which collectively and dramatically reduce the cost and complexity of building large airframes.
The ACCA's large composite sections are essentially formed, cured and bonded together in room-sized ovens, instead of using expensive autoclaves, which use a combination of heat and high pressure. Out-of-autoclave curing of large, unitized and co-bonded structures minimizes part count.
"ACCA is the capstone test of integrating these composite affordability initiative principles all the way from conceptual design through certification and flight," Mr. Shenk said.
The ACCA test aircraft is laden with more than 600 sensors and accelerometers to measure stresses on its structure. Upcoming tests will focus on establishing the flight envelope of the ACCA to baseline its flight performance and validate predicted structural performance.
"Accurately predicting structural behavior in the flight environment is a key step in establishing the eligibility of the technologies for transition into future programs, to fully realize the cost savings demonstrated by the ACCA," Mr. Shenk said.