| This electronic flyer highlights
our capabilities and activities in
Impact Assessment on Safety Structures and Aircraft Components.
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For additional
information, e-mail
Scott A. Mullin, Southwest Research Institute®. |
Impact Assessment on Safety Structures and Aircraft Components 
Southwest
Research Institute® (SwRI®) conducts a wide variety of safety-related impact
tests for many applications, projectiles, and test specimens: aircraft
components, bird impact resistance, engine failure fragments, and foreign object
damage to many different structural and shielding components. SwRI maintains
three ballistic gun systems that launch a large variety of projectile types and
shapes at speeds from 10 ft/s to over 2000 ft/s. The Large Compressed Gas Gun
Facility is capable of performing bird impacts from 240-knot commercial aircraft
FAA certification to 550+ knot Air Force canopy qualification testing.
Projectiles, test specimens and sabots are often designed, constructed and
tested at SwRI to meet the specific requirements of clients. A large suite of
state-of-the-art instrumentation and computer simulation codes support the
experimental facilities.
Capabilities
- Launch of projectiles from 0.1 to 15 inches in diameter (larger if
required)
- Impact speeds from 10 ft/s to over 2000 ft/s
- High-speed digital imaging of impacts up to 100,000,000 frames per
second
- Nicolet Multipro© high-speed data acquisition up to 200 MHz
- Test fixture fabrication
- Institute ISO-compliant QA
- Computer impact simulation
- Temperature control from –50°F to 150°F
- Gelatin and bird projectile testing
- Sabot design
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65-lb fragment-simulating projectile about
to impact Lexan shield design
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F16 canopy deflecting under impact by a
4-lb projectile at 550 knots
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Experience
- FAA bird strike certification testing at 240–280 knots
- Air Force bird strike qualification testing at 240–550 knots
- Engine containment shield tests with irregularly shaped projectiles
- Pressure measurements at impact point; correlation to simulations
- Impacts into Space Shuttle tiles with lightweight foam projectiles
- Impacts into personal protection shields, simulated plant equipment
- Shield and airframe design for impact survivability
Facilities
- Ballistics ranges with three compressed gas guns and over 20 barrels
- Three fully equipped instrumentation suites (one mobile)
- Target area for large components
- Mobile gun platform for easy targeting (yaw, pitch, waterline and
buttline)
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One-third of a jet engine compressor
packed in a sabot for launching. Complex sabots are often needed to launch
irregularly shaped projectiles.
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Civil aircraft fuselage undergoing
temperature-controlled bird strike testing. The insulated hood, hanging from
the crane, covers the fuselage for cooling or heating to the desired test
temperature and is raised moments before the projectile is fired at the
target.
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This flyer was published in April 2009. For more information about
Impact Assessment on Safety Structures and Aircraft Components, contact
Scott A. Mullin,
(210) 522-2340 or
Donald J. Grosch, (210)
522-3176,
Mechanical Engineering Division, Southwest
Research Institute, P.O. Drawer 28510, San Antonio, Texas 78228-0510.
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