Uncontrolled decompression (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Uncontrolled decompression" in English language version.

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  • Daidzic, Nihad E.; Simones, Matthew P. (March–April 2010). "Aircraft Decompression with Installed Cockpit Security Door". Journal of Aircraft. 47 (2): 490–504. doi:10.2514/1.41953. [A]t 40,000 ft (12,200 m), the International Standard Atmosphere (ISA) pressure is only about 18.8 kPa (2.73 psi), and the air temperatures are about −56.5 °C (217 K). The boiling temperature of water at this atmospheric pressure is about −59 °C (332 K). Above 63,000 ft or 19,200 m (Armstrong line), the ISA environmental pressure drops below 6.3 kPa (0.91 psi) and the boiling temperature of water reaches the normal human body temperature (about 37 C). Any prolonged exposure to such an environment could lead to ebullism, anoxia, and ultimate death, after several minutes. These are indeed very hostile conditions for human life.

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  • "AC 61-107A – Operations of aircraft at altitudes above 25,000 feet msl and/or mach numbers (MMO) greater than .75" (PDF). Federal Aviation Administration. 2007-07-15. Retrieved 2008-07-29.
  • "Chapter 7: Aircraft Systems". Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25B ed.). Federal Aviation Administration. 2016-08-24. p. 36. Archived from the original on 2023-06-20.
  • "AC 61-107A - Operations of aircraft at altitud above 25,000 feet MSL and/or mach numbers (MMO) greater than .75" (PDF). Federal Aviation Administration. July 15, 2007.
  • "FAA Historical Chronology, 1926–1996" (PDF). Federal Aviation Administration. 2005-02-18. Archived from the original (PDF) on 2008-06-24. Retrieved 2008-09-01.
  • "FAA historical chronology, 1926–1996" (PDF). Federal Aviation Administration. 2005-02-18. Archived from the original (PDF) on 2008-06-24. Retrieved 2008-07-29.
  • "Advisory Circular 61-107" (PDF). FAA. pp. table 1.1.

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  • "Columbia Crew Survival Investigation Report" (PDF). NASA.gov. 2008. pp. 2–90. The 51-L Challenger accident investigation showed that the Challenger CM remained intact and the crew was able to take some immediate actions after vehicle breakup, although the loads experienced were much higher as a result of the aerodynamic loads (estimated at 16 G to 21 G).5 The Challenger crew became incapacitated quickly and could not complete activation of all breathing air systems, leading to the conclusion that an incapacitating cabin depressurization occurred. By comparison, the Columbia crew experienced lower loads (~3.5 G) at the CE. The fact that none of the crew members lowered their visors strongly suggests that the crew was incapacitated after the CE by a rapid depressurization. Although no quantitative conclusion can be made regarding the cabin depressurization rate, it is probable that the cabin depressurization rate was high enough to incapacitate the crew in a matter of seconds. Conclusion L1-5. The depressurization incapacitated the crew members so rapidly that they were not able to lower their helmet visors.

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  • Bason R, Yacavone DW (May 1992). "Loss of cabin pressurization in U.S. Naval aircraft: 1969–90". Aviat Space Environ Med. 63 (5): 341–345. PMID 1599378.
  • Brooks CJ (March 1987). "Loss of cabin pressure in Canadian Forces transport aircraft, 1963–1984". Aviat Space Environ Med. 58 (3): 268–275. PMID 3579812.

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