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Impact Assessment on Safety Structures and Aircraft Components

 

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  image of 65-lb fragment-simulating projectile about to impact Lexan shield design
 

65-lb fragment-simulating projectile about to impact Lexan shield design

A wide variety of safety-related impact tests for many applications, projectiles, and test specimens are conducted at Southwest Research Institute (SwRI), including:

  • Aircraft components

  • Bird impact resistance

  • Engine failure fragments

  • Foreign object damage

  • Structural components

  • 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.

  image of one-third of a jet engine compressor packed in a sabot for launching. Complex sabots are often needed to launch irregularly shaped projectiles
 

One-third of a jet engine compressor packed in a sabot for launching. Complex sabots are often needed to launch irregularly shaped projectiles.

 

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.


Impact Assessment Capabilities

  • Launch of projectiles from 0.1 to 15 inches in diameter (larger if required)

  • Impact speeds from 10 ft/s to more than 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

  • SwRI ISO-compliant QA

  • Computer impact simulation

  • Temperature control from -50°F to 150°F

  • Gelatin and bird projectile testing

  • Sabot design

image of F16 canopy deflecting under impact by a 4-lb projectile at 550 knots

F16 canopy deflecting under impact by a 4-lb projectile at 550 knots


Impact Assessment 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

 

Impact Assessment Facilities

  image of 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
 

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.

  • Ballistics ranges with three compressed gas guns and more than 20 barrels

  • Three fully equipped instrumentation suites (one mobile)

  • Target area for large components

  • Mobile gun platform for easy targeting

  • Yaw

  • Pitch

  • Waterline

  • Buttline


Ballistics and Explosives Range

SwRI operates and maintains the Ballistics and Explosives Range on the San Antonio campus. This 10-acre facility permits a wide variety of experimental programs to be conducted, including:

  • Explosive loading

  • Hazards evaluation and mitigation

  • Foreign object damage

  • Ballistic impact

  • Armor testing

  • Hypervelocity impact

SwRI technicians provide expert support for handling explosives, firing gas and powder guns, and collecting high-rate electronic data. A complement of equipment, including an on-site machine shop, digital data acquisition and transient recorders, high-speed imaging equipment, and data processors, supports range activities.


For more information about impact assessment on safety structures and aircraft components capabilities at SwRI or how you can contract with SwRI, please contact Scott A. Mullin at smullin@swri.org or (210) 522-2340.

 

Contact Information

Scott A. Mullin

Impact Assessment on Safety Structures and Aircraft Components

(210) 522-2340

smullin@swri.org

Related Terminology

impact assessment

safety structures

aircraft components

bird-strike resistance

compressor failure

safety shielding

shrapnel

aircraft impact survivability

compressed gas guns

FAA FAR 25.775

ASTM F330

foreign object damage

FOD

engine fragment containment

containment rings

canopy testing

aircraft leading

edge testing

impact survivability

homeland security

Related Information

image of Impact Assessment on Safety Structures and Aircraft Components flyer
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Southwest Research Institute® (SwRI®), headquartered in San Antonio, Texas, is a multidisciplinary, independent, nonprofit, applied engineering and physical sciences research and development organization with 11 technical divisions.

October 01, 2008