After a month of tests in a University of
Washington water tunnel, Boeing engineers have identified a trio of
design options to enhance the aerodynamic performance of a key component
of the Airborne Laser (ABL) program: the 104-inch nose turret that aims
the weapon's laser at theater ballistic missiles to destroy them in
flight.
The ABL weapon system will use a high-energy, chemical oxygen iodine
laser (COIL) mounted on a modified 747-400F aircraft to shoot down
theater ballistic missiles in their boost phase. It will protect
civilian and key military assets from attack by missiles such as the
Scuds used by Iraq during the Persian Gulf War.
"The water tunnel tests worked very well for us in three major ways,"
said Boeing engineer Victor Buonadonna. "First, we confirmed that our
existing design concept will work as conceived. Second, we reduced the
number of designs we will study in wind tunnels later this year from 15
down to the three that showed the greatest promise. And third, we got
the information at very low cost by using the water tunnel."
Buonadonna said water tunnel tests ending in June were completed for
about $25,000 compared to wind tunnel costs which average between
$20,000 to $30,000 per day.
Water tunnels are ideal for investigating fluid flow over solid
spherical surfaces - in this case the turret to be mounted on the nose
of a modified Boeing 747-400 Freighter chosen for the weapon system
platform. Through observation of the colored streams of water as they
flow over the structure, engineers can identify problems with the flow
and change the structure's shape to correct them.
In the tests, Boeing confirmed what earlier analysis had shown: in
certain turret positions, the air flow - called the "boundary layer" -
separated from the turret surface and created a turbulent "shear layer."
"The turbulence degrades the laser beam quality when the laser aims
through it," Buonadonna said. "That results in a blurred spot on the
target that increases the time required to destroy the target. The water
tunnel studies allowed us to test many configurations for reducing the
turbulence and improving beam quality using a concept called 'passive
flow control'," he added.
Buonadonna explained that the concept was suggested in 1995 by Dr. Bob
Breidenthal, University of Washington aerodynamics professor, who was
working with Boeing in a series of ABL-related wind tunnel tests. In
those tests, the passive flow control concept proved so effective that
it became the baseline for the Boeing ABL turret aerodynamic design.
The concept employs suction at the base of the turret to eliminate or
decrease the shear layer. That suction is provided by a "speed bump"
that produces a partial vacuum behind it, "pulling" the boundary layer
back onto the aft portion of the spherical turret. The system is passive
in that no mechanical pump is required.
"With the successful conclusion of the water tunnel tests, we are ready
to focus the upcoming wind tunnel tests on the three designs,"
Buonadonna said. He added that Boeing is "very confident that the
November wind tunnel tests will finalize the turret design and produce
the design efficiencies we want."
Boeing is responsible for the aerodynamic design of the turret, its
attachment to the nose of the modified 747-400F and integrating the
weapon system onto the aircraft. The optics and control of the laser
beam that fires through the turret's window are the responsibility of
Lockheed Martin. Northrop Grumman is designing and producing the weapon system's
powerful laser.
Milestones
- May 1994
- Team ABL (Boeing, Lockheed Martin and Northrop Grumman) and Rockwell
awarded 33-month, Concept Definition contracts
- July 8, 1996
- Team ABL submits response to RFP
- Nov. 15, 1996
- Air Force selects Team ABL for Program Definition and Risk Reduction
(PDRR) phase of program.
- 1996-2000
- PDRR phase one (build one ABL weapon system)
- 2000-2001/2
- PDRR phase two (flight test & demonstration)
- 2001/2-2004
- Engineering Manufacturing and Development (EMD)
- 2004-2008
- Production
(Initial Operational Capability -- 3 aircraft 2005/6; Full Operational
Capability -- 7 aircraft 2008)