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	+ ATP Home		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. + View Enlargement Pneumatic Icing Boot Firing High speed video footage of an aircraft wing's pneumatic icing boot firing to shed ice build-up. + View Video (Flash) C95-3918 PFM powered force model rotor. This image shows one possible type of ice accretion that the Icing Tunnel can produce. + View Enlargement C98-1749 Bell 609 spinner inlet icing model. Technicians taking measurement of ice accretions after an icing test. + View Enlargement Water Droplet Impact Side view of high-speed video of water droplet impacting front edge of airfoil in the NASA Glenn Icing Research Tunnel's test section. + View Video (Flash) C2000-1836 Technicians pose with the ERJ-170 airfoil set up for testing the IRT. + View Enlargement NASA's ATP Program Read about one of the largest, most versatile and comprehensive set of testing facilities in the nation. + View the fact sheet (PDF) Icing Research Tunnel + View the fact sheet (PDF) GRC Research Facilities Find out more about the research facilities at NASA's Glenn Research Center + View the site Get Flash Player + Download now "The right facility at the right time" - NASA Aeronautics Test Program
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