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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35 to 40 feet wide. Although it was difficult to maintain the correct liquid water content and droplet size with the HISS system, the tests still provided significant information about the inflight performance of the de-icing system. Perhaps the most important result of the HISS tests related to the durability of the Estane boots. After 6 hours of artificial rain testing behind the tanker, there was no detectable erosion of the Estane6. Erosion testing continued at Fort Rucker, Alabama, where the Estane boots withstood 10 hours of sand erosion. However, 10 hours of flying in natural rain required four sepa- rate blade repairs due to the pitting and chunking of the Estane. By 1987, the conclusion had been reached that the Goodrich boot was a feasible rotor-protection system, but that additional field tests were required to gain more experience with the erosion problem.7 Far more promising than the Goodrich boot as an innovative ice-protection system for both helicopters and fixed-wing aircraft was the Electro-Impulse De-Icing (EIDI) system that occupied a good deal of NASA’s attention during the 1980s. The use of electro-magnetic energy as an impulse force to remove ice had been first suggested in 1937 by Rudolf Goldschmidt, a German national who was living in London. Although Goldschmidt had obtained a patent for his concept, he apparently had never attempted to build a device to test his ideas. The concept had emerged again in the mid-1960s in the Soviet Union. I. I. Levin of the Ministry of Power and Electricity had published a paper on the possibility of employing electro-impulse force to remove frozen and sticky material from bunkers, transformer boxes, and other surfaces.8 The Soviets had installed the system on an Ilyushin IL-18 transport in the 1970s, then sent salesmen to Western nations to market the concept. They had shown a film of a wing with heavy icing. In an instant, the ice had disappeared. Although it had been impossible to tell whether the wing was attached to an airplane in flight or had been pho- tographed in a wind tunnel, viewers had nonetheless been impressed. The Soviets had refused to provide any further details, had referred interested parties to Levin’s article, and had asked for $500,000 to develop the system for any aircraft. The Russians had not gotten their $500,000, but their visit had sparked interest in the system in Western Europe and in the United States. The French had attempted to put an electro-impulse system on an Alpha Jet, but it had not worked well. The British Back in Business 6 “NASA’s Rotorcraft Icing Research Program.” The HISS system is described in the FAA’s Aircraft Icing Handbook, vol. 2, ch. IV. 7 “NASA’s Rotorcraft Icing Research Program.” 8 For the EIDI story, see G. M. Zumwalt, R. L. Schrag, W. E. Bernhart, and R. A. Friedberg, “Electro-Impulse De-Icing: Testing, Analysis and Design,” NACA CR 4175 (September 1988); and Zumwalt to Leary, 30 August 2000. 85

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