Transformed X-48c Flies Successfully

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Aug. 7, 2012

Michael Braukus 
Headquarters, Washington      
202-358-1979 
michael.j.braukus@xxxxxxxx 

Gray Creech 
Dryden Flight Research Center 
661-276-2662 
gray.creech-1@xxxxxxxx 

Tom Koehler 
Boeing Research & Technology Communications 
425-373-2921 
thomas.j.koehler@xxxxxxxxxx 


RELEASE: 12-259

TRANSFORMED X-48C FLIES SUCCESSFULLY

Edwards AFB, Calif. -- The remotely piloted X-48C aircraft 
successfully flew for the first time Tuesday at Edwards Air Force 
Base in California's Mojave Desert. 

The aircraft, designed by The Boeing Co. and built by Cranfield 
Aerospace Limited of the United Kingdom, is flying again in 
partnership with NASA. The new X-48C model, which was formerly the 
X-48B Blended Wing Body aircraft, was modified to evaluate the 
low-speed stability and control of a low-noise version of a notional, 
future Hybrid Wing Body (HWB) aircraft design. The HWB design stems 
from concept studies being conducted by NASA's Environmentally 
Responsible Aviation project of future potential aircraft designs 20 
years from now. 

"We are thrilled to get back in the air to start collecting data in 
this low-noise configuration," said Heather Maliska, X-48C project 
manager at NASA's Dryden Flight Research Center. "Our dedicated team 
has worked hard to get the X-48C off the ground for its first flight 
and we are excited learning about the stability and control 
characteristics of this low-noise configuration of the blended wing 
body." 

Primary changes to the C model from the B model, which flew 92 flights 
at Dryden between 2007 and 2010, were geared to transforming it to an 
airframe noise-shielding configuration. External modifications 
included relocating the wingtip winglets inboard next to the engines, 
effectively turning them into twin tails. The aft deck of the 
aircraft was extended about 2 feet to the rear. Finally, the project 
team replaced the X-48B's three 50-pound thrust jet engines with two 
89-pound thrust engines. 

Because handling qualities of the X-48C will be different from those 
of the X-48B, the project team developed flight control system 
software modifications, including flight control limiters to keep the 
airplane flying within a safe flight envelope. This will enable a 
stronger and safer prototype flight control system suitable for 
future full-scale commercial hybrid or blended wing aircraft. 

"We are very pleased to begin flight tests of the X-48C," said Mike 
Kisska, Boeing X-48C project manager. "Working with NASA, we've 
successfully passed another milestone in our work to explore and 
validate the aerodynamic characteristics and efficiencies of the 
blended wing body concept." 
Additionally, the upc 
oming flight experiments with the X-48C will help researchers further 
develop methods to validate the design's aerodynamics and control 
laws, including a goal of reducing aerodynamic drag through engine 
yaw control tests. 

During the planned second block of flight testing this fall, NASA will 
test engine yaw control software incorporated in the X-48C's flight 
computer. This research will use asymmetric engine thrust to create 
yaw, or nose left or right movements, for trim and for relatively 
slow maneuvers. 
NASA's Aeronautics Research Mission Directorate and Boeing are funding 
the X-48 technology demonstration research effort, which supports 
NASA's goals of reduced fuel burn, emissions and noise. 

The X-48C retains most dimensions of the B model, with a wingspan just 
longer than 20 feet, and a weight of about 500 pounds. The aircraft 
has an estimated top speed of about 140 mph, and a maximum altitude 
of 10,000 feet. 

The Air Force Research Laboratory, Dayton, Ohio, also is a member of 
the project team. 

For more information about the Aeronautics Research Mission 
Directorate, visit: 

http://www.aeronautics.nasa.gov 

	
-end-



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