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The predawn darkness on a cool Florida night was shattered by the ignition of nine Merlin engines on a SpaceX Falcon 9 rocket. The thrust of the engines shook the ground miles away. From a distance, the rocket appeared to slowly rise above the horizon. For the cargo onboard, the launch was anything but gentle, as the ignition of liquid oxygen generated more than 1.5 million pounds of force. After the rocket had been out of sight for several minutes, the booster dramatically returned to Earth with several sonic booms in a captivating show of engineering designed to make space travel less expensive and more sustainable.
M. W. Mahoney, N. E. Paton
Nuclear Technology | Volume 23 | Number 3 | September 1974 | Pages 290-297
Technical Paper | Material | doi.org/10.13182/NT74-A15921
Articles are hosted by Taylor and Francis Online.
Fatigue crack growth rates of Types 316 and 321 stainless steel were studied as a function of stress intensity, temperature, relative humidity, and gas environment. At 25°C it was shown that humidity in the presence of oxygen will accelerate crack growth rates by a factor of ∼1.7, as compared to an inert environment such as dry nitrogen or argon. In addition, a threshold level is implied for the effect of humidity above which further increases in moisture content have no additional influence on crack growth rates. At 649°C an air environment was found to increase crack growth rates by factors of ∼22 and ∼5 for Types 316 and 321 stainless steel, respectively, over rates determined in either argon or nitrogen. Crack growth rates in nitrogen and argon at 649°C were comparable to crack growth rates at 25°C, leading to the conclusion that increased growth rates observed at 649°C in air are principally a result of environmental interactions with the crack front rather than a result of reduced mechanical properties at 649°C. These results also show that Type 321 stainless steel is less susceptible than Type 316 to aggressive environments at 649°C such as room air, suggesting that Type 321 might be a better choice of material for some elevated temperature applications. Fractography of specimens tested at 649°C revealed the absence of striation formation for specimens tested in inert environments, while pronounced striations were found in environments such as air.