History of NASA Icing Research Tunnel

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History of NASA Icing Research Tunnel ( history-nasa-icing-research-tunnel )

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required to remove the ice was measured with a load cell. Reich could calculate adhesion force with a simple mathematical formula. In these tests, the Dow coating also came out on top, displaying fairly repeatable adhesive strength that increased only slightly with a number of ice removals. While the Goodrich tests were encouraging, Anderson knew that impact ice had dif- ferent physical characteristics than static ice. In an attempt to obtain quantifiable results with impact ice in the IRT, he employed in the next series of tests a shear rig that had been developed at the University of Akron by R. L. Scavuzzo and M. L. Chu. Based on the earlier NASA device, it used a 1-inch-diameter cylinder that would be coated with test material and mounted inside a thin sleeve. A window that was cut from the sleeve exposed a portion of the cylinder to the icing cloud. Ice accreting on the sleeve bonded the cylinder to the sleeve at the window. Once the ice had accreted, the cylinder-sleeve assembly was removed and placed on a stand. The cylinder was then forced through the sleeve by a hydraulic press acting through a load cell. The force required to free the cylinder was recorded on a strip chart. Anderson soon found that the mechanism suffered from two major problems. Ice sometimes caused adjoining cylinder-sleeve assemblies to stick together, making disas- sembly difficult. Also, the cylinder often separated from the sleeve when removed from the test stand, especially with low adhesion coatings. As a result, no measurements could be obtained. In the end, Anderson considered the data that he obtained from the shear rig tests to be unreliable. NASA technicians managed to devise a test stand that permitted shear-force meas- urements to be made in the tunnel without disturbing the coating specimens. Two coatings stood out in the subsequent tests. Both the Dow “Anti-Stick” coating and a fluoropolymer-based DuPont coating reduced adhesive strength by 30 to 50 percent. These results were confirmed in the Goodrich tunnel. At this point, NASA concluded its work on the ice-phobic project, leaving Goodrich and the chemical companies to develop further a practical low-adhesive coating.12 One of the most innovative uses of the IRT during the 1990s came with tests of the effects of lightning strikes on radomes. Because radomes were constructed from non- electrically conducting materials, they were vulnerable to being punctured or shattered by lightning strikes. To minimize this danger, radomes initially had been fitted with an arrangement of solid metal bars, called diverters, that would conduct the lightning safely to the airframe. Newer protection devices—segmented diverters—accomplished the same purpose but caused less interference with radar performance. Verification of the The 1990s 12 Anderson interview; David N. Anderson and Allen D. Reich, “Tests of the Performance of Coatings for Low Ice Adhesion,” NASA TM 107399 (1997). 161

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