|
|
 |
| |
|
|
 |
| |
 |
| |
J.D. Harrington
Headquarters, Washington
Phone: 202-358-5241
Gray Creech
Dryden Flight Research Center, Edwards, California
Phone: 661-276-2662
|
July 26, 2007
|
RELEASE: 07-165
|
X-48B BLENDED WING BODY RESEARCH AIRCRAFT TAKES FIRST FLIGHT
Image to right: The X-48B Blended Wing Body research aircraft flew for the first time last week at NASA’s Dryden Flight Research Center. NASA Photo.
WASHINGTON – The collaborative efforts of the Boeing Co. of Chicago,
Ill., NASA’s Fundamental Aeronautics Program, and the Air Force Research
Laboratory at Wright Patterson Air Force Base, Ohio culminated on the
first flight of the X-48B Blended Wing Body research aircraft on July
20, 2007. The experienced flight research team kept a watchful eye as
the 21-foot wingspan, 500-pound, remotely piloted test vehicle took off
for the first time at 8:42 a.m. PDT and climbed to an altitude of 7,500
feet before landing 31 minutes later.
"Friday's flight marked yet another aviation first achieved by a very
hard-working Boeing, NASA, AFRL, and Cranfield team," said Gary
Cosentino, Dryden's Blended Wing Body project manager for NASA’s
Subsonic Fixed Wing Project. "The X-48B flew as well as we had
predicted, and we look forward to many productive data flights this
summer and fall."
In addition to hosting the X-48B flight test and research activities,
NASA provided engineering and technical support -- expertise garnered
from years of operating cutting-edge air vehicles. NASA assisted with
the hardware and software validation and verification process, the
integration and testing of the aircraft systems, and the pilot's ground
control station. NASA's range group provided critical telemetry and
command and control communications during the flight, while the flight
operations group provided a T-34 chase aircraft and essential flight
scheduling. Photo and video support completed the effort.
The Subsonic Fixed Wing Project team under the Fundamental Aeronautics
Program has long supported the development of the blended wing body
concept. It has participated in numerous collaborations with Boeing, as
well as several wind tunnel tests for different speed regimes. The team
is focused on researching the low-speed characteristics of the design
and expanding its flight envelope beyond the limits of current
capabilities.
NASA is interested in the potential benefits of the aircraft – increased
volume for carrying capacity, efficient aerodynamics for reduced fuel
burn, and, possibly, significant reductions in noise due to propulsion
integration options. In these initial flights, the principal focus is to
validate prior research on the aerodynamic performance and
controllability of the shape, including comparisons of the flight data
with the extensive wind-tunnel database.
The X-48B flight test vehicles were designed to gather detailed
information about the stability and flight-control characteristics of
the blended wing body design, especially during takeoffs and landings.
The blended wing body design resembles a flying wing, but differs in
that the wing blends smoothly into a wide, flat, tailless fuselage. This
fuselage blending provides additional lift with less drag than a
traditional circular fuselage, translating into reduced fuel use at
cruise conditions. Since the engines can be mounted on the top surface
of the configuration there is a potential for significant noise
reduction on the ground.
Three turbojet engines enable the composite-skinned, 8.5 percent scale
vehicle to fly up to 10,000 feet and 120 knots in its low-speed
configuration. The aircraft is flown remotely from a ground control
station in which the pilot uses conventional aircraft controls and
instrumentation while looking at a monitor fed by a forward-looking
camera on the aircraft.
Up to 25 flights are planned to gather data in these low-speed flight
regimes. Then, the X-48B may be used to test the aircraft's low-noise
and handling characteristics at transonic speeds.
Two X-48B research vehicles were built by Cranfield Aerospace Ltd., in
Bedford, England, in accordance with Boeing requirements. The vehicle
that flew on July 20 is Ship 2, which also was used for ground and taxi
testing. Ship 1, a duplicate, completed extensive wind tunnel testing in
2006 at the Full-Scale Tunnel at NASA's Langley Research Center in
Hampton, Va. Ship 1 will be available for use as a backup during the
flight test program.
- end -
|
 |
|
|