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Oxygen Fires
from
http://astronautix.com/thisday/sepber10.htm#BORN "1962 - • Fire in a simulated Air Force space cabin Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. • Fire broke out in a simulated space cabin at the Air Force School of Aerospace Medicine, Brooks Air Force Base, Tex., on the 13th day of a 14-day experiment to determine the effects of breathing pure oxygen in a long-duration space flight. One of the two Air Force officers was seriously injured. The cause of the fire was not immediately determined. The experiment was part of a NASA program to validate the use of a 5 psia pure oxygen atmosphere for the Gemini and Apollo spacecraft." Yet the continued to use a pure oxygen atmosphere until Apollo1 five years later? -- Gareth Slee |
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Oxygen Fires
Gareth Slee wrote: from http://astronautix.com/thisday/sepber10.htm#BORN "1962 - · Fire in a simulated Air Force space cabin Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. · Fire broke out in a simulated space cabin at the Air Force School of Aerospace Medicine, Brooks Air Force Base, Tex., on the 13th day of a 14-day experiment to determine the effects of breathing pure oxygen in a long-duration space flight. One of the two Air Force officers was seriously injured. The cause of the fire was not immediately determined. The experiment was part of a NASA program to validate the use of a 5 psia pure oxygen atmosphere for the Gemini and Apollo spacecraft." Yet the continued to use a pure oxygen atmosphere until Apollo1 five years later? -- Gareth Slee From a 1964 NASA report: Space-cabin atmospheres. part ii - fire and blast hazards a literature review Roth, E. M. NASA Center for AeroSpace Information (CASI) NASA-SP-48 , 19640101; Jan 1, 1964 Fire and blast hazards in space cabin atmospheres Accession ID: 64N20744 Document ID: 19640010830 http://ntrs.nasa.gov/archive/nasa/ca...964010830..pdf -Rusty |
#3
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Oxygen Fires
In article ,
Gareth Slee wrote: "1962 - • Fire broke out in a simulated space cabin at the Air Force School of Aerospace Medicine, Brooks Air Force Base, Tex., on the 13th day of a 14-day experiment to determine the effects of breathing pure oxygen in a long-duration space flight... The experiment was part of a NASA program to validate the use of a 5 psia pure oxygen atmosphere for the Gemini and Apollo spacecraft." Yet the continued to use a pure oxygen atmosphere until Apollo1 five years later? They continued to use a pure oxygen atmosphere *in flight* -- that's the 5-psi atmosphere referred to -- throughout Apollo. There were important reasons for this; it was not just some careless whim. The conditions of the simulated cabin were not considered representative of actual spaceflight or of actual space hardware. Most everyone understood that there was some fire hazard associated with the in-flight atmosphere, but the combination of free fall (suppressing convection) and an effort to exclude ignition sources from the Apollo cabin was thought sufficient to control the hazard. The issue was not ignored; serious attention was given to fire hazards during planning. Unfortunately, the combination of a poorly-run development process and a steady stream of uncontrolled engineering changes undermined this somewhat. There was much more flammable material in the cabin than had originally been intended, and the already-optimistic goal of excluding ignition sources was compromised by sloppy workmanship. But the big flaw was simply that all the work on fire hazards had focused on *in-flight* fires. Nobody thinking about fire prevention noticed that Apollo testing and ground operations were being done with pure oxygen at 16 psi, which is *much* more dangerous than 5 psi, especially in 1 G. (There were again real reasons for this choice of atmosphere, but people would nevertheless have thought twice about it if the added hazard had been noticed.) After the fire, they *didn't* change the in-flight atmosphere, because the technical reasons for pure oxygen there remained compelling. They did change a fundamental assumption: ignition sources were now assumed to be present, so fire could start, but it must not spread enough to be dangerous. Flammable materials were eliminated wherever possible, and drastically restricted if they could not be eliminated (there simply weren't any non-flammable substitutes for some things). And after a lot of effort, they ended up having to accept a different cabin atmosphere (the suits still had pure oxygen in them) for ground operations, with a transition to pure oxygen during ascent, because fireproofing the cabin well enough for 16-psi oxygen just didn't end up being practical. -- spsystems.net is temporarily off the air; | Henry Spencer mail to henry at zoo.utoronto.ca instead. | |
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Oxygen Fires
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Oxygen Fires
David Lesher writes:
How did they avoid killing the crew with that 16psi pure O2? ISTM there are lots of nasty side effects of too much O2...and 100% 16ps is way too much... Oxygen toxicity at 16 psi of 100% O2 don't show up for quite some time (12-16 hours). By then, they'd already be launched and running at lower pressure (around 4 psi, IIRC). -- Richard W Kaszeta http://www.kaszeta.org/rich |
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Oxygen Fires
In article ,
David Lesher wrote: ...they ended up having to accept a different cabin atmosphere (the suits still had pure oxygen in them) for ground operations... How did they avoid killing the crew with that 16psi pure O2? ISTM there are lots of nasty side effects of too much O2...and 100% 16ps is way too much... As witness hospital oxygen tents, breathing pure oxygen at around 1 atm pressure for a little while is not grievously harmful. It's not something you want to do for weeks on end if you can avoid it, but the Apollo crews typically got it for only a few hours. (E.g., on a launch day, between suiting up and the middle of ascent.) They had to pre-breathe pure oxygen for a while before launch anyway, to flush the nitrogen out of their bodies, since they were going to be decompressing to 5 psi during ascent. (And might have to decompress further, to suit operating pressure, in the event of (say) cabin damage during initial docking with the LM.) -- spsystems.net is temporarily off the air; | Henry Spencer mail to henry at zoo.utoronto.ca instead. | |
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Oxygen Fires
On 11 Sep 2006 07:38:52 -0500, Richard Kaszeta
wrote: ISTM there are lots of nasty side effects of too much O2...and 100% 16ps is way too much... Oxygen toxicity at 16 psi of 100% O2 don't show up for quite some time (12-16 hours). By then, they'd already be launched and running at lower pressure (around 4 psi, IIRC). Weren't they in their suits for launch, anyway? Brian |
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Oxygen Fires
Henry Spencer wrote:
After the fire, they *didn't* change the in-flight atmosphere, because the technical reasons for pure oxygen there remained compelling. They did change a fundamental assumption: ignition sources were now assumed to be present, so fire could start, but it must not spread enough to be dangerous. Flammable materials were eliminated wherever possible, and drastically restricted if they could not be eliminated (there simply weren't any non-flammable substitutes for some things). And after a lot of effort, they ended up having to accept a different cabin atmosphere (the suits still had pure oxygen in them) for ground operations, with a transition to pure oxygen during ascent, because fireproofing the cabin well enough for 16-psi oxygen just didn't end up being practical. Thank you Henry for clearing up my misconceptions. -- Gareth Slee |
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Oxygen Fires
"Gareth Slee" wrote in message . .. Yet the continued to use a pure oxygen atmosphere until Apollo1 five years later? That's why they were no-smoking flights. With the pure oxygen added to the excessive hydrogen in the water produced by the fuel cells... That's the *real* cause of Apollo 13- with those harsh arc lights simulating the sun, one of the stage hands lit up too close to the CM simulator, and .... |
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Oxygen Fires
Brian Thorn wrote: Weren't they in their suits for launch, anyway? Remember, inside a cabin pressurized to 16 psi, any suit would be pressurized to at least 16 psi as well (for comfort if nothing else), and also at 100% oxygen--otherwise, why bother? Also, IIRC the 16 psi was for a leak check, and was depressurized back to 14.7 psi sea level pressure for launch. John Charles Houston, Texas |
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