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Icing Research Tunnel Video
View an in-depth video about the capabilities of the Icing Research Tunnel (10 min, 30 sec.)
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C2008-4282
Wichita University - IMS - Sprint 727 Inlet - Electro-Expulsive De-Icing System Test (EEDS)
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C2008-1526
Cessna Tail Wing Section being tested in the Icing Research Tunnel (IRT).
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C2008-714
General Atomics - Predator B Wing Section - Leading edge de-icing evaluation.
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C2008-601
S-3 Viking one-third scale wing section in the IRT.
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C2008-521
General Atomics - Predator B Model mounted in the IRT test section.
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C2007-114
View of the Kelly Aerospace 727 inlet anti-icing model mounted in the IRT test section.
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C87-1127
The powerful fan and motor at the heart of the Icing Research Tunnel is capable of producing continuous airspeeds up to 395 mph.
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C2007-459
The FJ33 inlet from Williams International being tested in the Icing Research Tunnel.
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C95-3918
PFM powered force model rotor. This image shows one possible type of ice accretion that the Icing Tunnel can produce.
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C98-1749
Bell 609 spinner inlet icing model. Technicians taking measurement of ice accretions after an icing test.
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C2000-1836
Technicians pose with the ERJ-170 airfoil set up for testing in the IRT.
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