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NRC moves forward with sunset of aircraft impact assessment rule
The Nuclear Regulatory Commission has sunset its aircraft impact assessment rule for 2027, as NRC staff have addressed several of the public comments considered “significant and adverse” that prompted the agency this past winter to temporarily delay the sunsetting move.
The final rule, which was published in the Federal Register on Wednesday, addressed some of the more contentious concerns raised by the public. It sets a conditional sunset date of April 8, 2027, “unless the NRC determines that the cessation deadline should be extended to a date not more than 5 years in the future after offering the public an opportunity to provide input on the costs and benefits of this section and considering that input.”
Yassin A. Hassan, Laxminarayan L. Raja
Nuclear Technology | Volume 104 | Number 1 | October 1993 | Pages 76-88
Technical Paper | Heat Transfer and Fluid Flow | doi.org/10.13182/NT93-A34871
Articles are hosted by Taylor and Francis Online.
A computational investigation of experiments involving the condensation phenomenon in the presence of noncondensable gases was performed. TheRELAP5/MOD3 thermal-hydraulic code was utilized for this analysis. Two separate-effects experiments were studied, which are relevant to actual situations encountered in the industry. The first experiment involved condensation of steam in an inverted U-tube when nitrogen is present. A constant flow of steam was injected into the U-tube and condensed along its surface. The condensing length was a function of the injected nitrogen rate and the secondary temperature. The code predicted an active condensation zone with unimpeded heat transfer and a passive zone with no heat transfer. The lengths of these zones agree with the experimental data. The gas temperatures in the U-tube were favorably predicted except for a discrepancy where the calculated primary temperatures were lower than the secondary temperatures for several cases. Active nitrogen contents in the tube were underpredicted by the code. The second experiment investigated was the Massachusetts Institute of Technology’s steam condensation experiment. This experiment modeled the proposed containment cooling system for advanced reactors. Steam was generated in a vessel in which air was present. The steam in the steam-air mixture condensed on the surface of a cooled copper cylinder. Computational predictions of this experiment revealed that heat transfer coefficients vary with air fraction. Calculated heat transfer coefficients were compared with the data, and it was found that the results were better for higher system pressures than for lower pressures.