In this animation future astronauts return to the lunar surface.http://www.nasa.gov/multimedia/guide...
www.fricso.com FriCSo develops and provides advanced nanolayer-based technology for friction reducti...
Microsoft Unveils a "Hands On" Experience Microsoft is launching the first consumer surface computer...
The procedures used to clean the cubicle after dismissing the patient. Orig. air date: AUG 14 79
Microsoft Unveils a "Hands On" Experience Microsoft is launching the first consumer surface computer...
NASA |
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Views: (1501) Date: (Jun 1, 1984) Pages: () |
Abstract: Baseline burner rig hot corrosion with Udimet 700, Rene' 80; uncoated and with RT21, Codep, or NiCoCrAlY coatings were tested. Test conditions are: 900C, hourly thermal cycling, 0.5 ppm sodium as NaCl in the gas stream, velocity 0.3 Mach. The uncoated alloys exhibited substantial typical sulfidation in the range of 140 to 170 hours. The aluminide coatings show initial visual evidence of hot corrosion at about 400 hours, however, there is no such visual evidence for the NiCoCrAlY coatings. The turbine components show sulfidation. The extent of this distress appeared to be inversely related to the average length of mission which may, reflect greater percentage of operating time near ground level or greater percentage of operation time at takeoff conditions (higher temperatures). In some cases, however, the location of maximum distress did not exhibit the structural features of hot corrosion.