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A13 O2 Tank Rupture Was Not An Explosion
Recent quotes he
"After the explosion on the A13 SM..." "When power and heat were off after the exploson..." Years ago I had a discussion with someone who was on the A13 investigation board. He explained to me that the tank did not explode. It could more accurately be described as the cap getting blown off followed by O2 streaming away, the force of which tore away the SM panel and such. The tank rupture was just not violent enough to qualify as an explosion. Even in Ron Howard's movie, Lovell is shown looking outside as the O2 sprays off. Had the tank actually exploded, its contents would have been gone in one shot. (Along with Apollo 13, it is also popular to hear -51L, -107 and sometimes even A204 being referred to as an "explosion". Let's not mistake colloquialism for accurate descriptions of the failure modes.) ~ CT |
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A13 O2 Tank Rupture Was Not An Explosion
"Stuf4" wrote in message om... | | It could more accurately be described as the cap getting | blown off followed by O2 streaming away, the force of which tore away | the SM panel and such. Yes, "explosion" is the wrong word. However, gaseous O2 loss continued after the first tank failure because oxygen from the undamaged tank was leaking away through the damaged plumbing. There was no tank isolation valve at that time. -- | The universe is not required to conform | Jay Windley to the expectations of the ignorant. | webmaster @ clavius.org |
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A13 O2 Tank Rupture Was Not An Explosion
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A13 O2 Tank Rupture Was Not An Explosion
On Tue, 02 Sep 2003 23:56:55 -0400, Jan Philips
wrote: On 1 Sep 2003 22:52:24 -0700, (Stuf4) wrote: Years ago I had a discussion with someone who was on the A13 investigation board. He explained to me that the tank did not explode. I stand corrected. ....Do *not* stand corrected wherever this particular troll is concerned. Again, do a google on "~CT" or "Stuff4" and see just what sort of bull**** games he plays in his posts. Best bet is to killfile him and be done with him for all time. OM -- "No ******* ever won a war by dying for | http://www.io.com/~o_m his country. He won it by making the other | Sergeant-At-Arms poor dumb ******* die for his country." | Human O-Ring Society - General George S. Patton, Jr |
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A13 O2 Tank Rupture Was Not An Explosion
From Jud:
It could more accurately be described as the cap getting blown off followed by O2 streaming away, the force of which tore away the SM panel and such. The tank rupture was just not violent enough to qualify as an explosion. Even in Ron Howard's movie, Lovell is shown looking outside as the O2 sprays off. Had the tank actually exploded, its contents would have been gone in one shot. I thought that the oxygen on one tank immediately went to zero, and the other gradually went to zero. I would guess that the venting was from the later. Never hurts to go straight to the official word: "REPORT OF APOLLO 13 REVIEW BOARD" - http://tinyurl.com/m2nm (http://spacelink.nasa.gov/NASA.Proje...ard.Report.txt) "It is now clear that oxygen tank no. 2 or its associated tubing lost pressure integrity because of combustion within the tank, and that effects of oxygen escaping from the tank caused the removal of the panel covering bay 4 and a relatively slow leak in oxygen tank no. 1 or its lines or valves." [Compare/contrast "lost pressure integrity" versus "exploded". Toward the end of the report, the terminology they used is "pressure pulse".] "After the relatively slow propagation process ... took place, there was a relatively abrupt loss of oxygen tank no. 2 integ- rity. About 69 seconds after the pressure began to rise, it reached the peak recorded, 1008 psia, the pressure at which the cryogenic oxygen tank relief valve is designed to be fully open. Pressure began a decrease for 8 seconds, dropping to 996 psia before readings were lost." [NASA knows that pressure vessels are potential bombs. This one was designed to relieve extreme pressure in a non-catastrophic way: through designed pressure release mechanisms.] "27. Findings a. The pressure relief valve was designed to be fully open at about 1000 psi. b. Oxygen tank no. 2 telemetry showed a pressure drop from 1008 psia at 55:54:45 to 996 psia at 55:54:53, at which time telemetry data were lost. Determination This drop resulted from the normal operation of the pressure relief valve as verified in subsequent tests." * There's lots more excellent info in that report. I've distilled the sequence of events for anyone interested: ________ 55:52-:31 Master caution and warning triggered by low hydrogen pressure in tank no. 1. Alarm is turned off after 4 seconds. 55:52:58 Ground requests tank stir. 55:53:06 Crew acknowledges tank stir. .... 55:53:20 Oxygen tank no. 2 fans turned on. .... 55:53:22.757 1.2-volt decrease in ac bus 2 voltage. 55:53:22.772 11.1-amp rise in fuel cell 3 current for one sample. 55:53:36 Oxygen tank no. 2 pressure begins rise lasting for 24 seconds. .... 55:53:41.192 Stabilization control system electrical disturbance indicates a power transient. 55:54:00 Oxygen tank no. 2 pressure rise ends at a pressure of 953.8 psia. 55:54:15 Oxygen tank no. 2 pressure begins to rise. 55:54:30 Oxygen tank no. 2 quantity drops from full scale for 2 seconds and then reads 75.3 percent. 55:54:31 Oxygen tank no. 2 temperature begins to rise rapidly. 55:54:43 Flow rate of oxygen to all three fuel cells begins to decrease. 55:54:45 Oxygen tank no. 2 pressure reaches maximum value of 1008.3 psia. 55:54:48 Oxygen tank no. 2 temperature rises 40ø F for one sample (invalid reading). 55:54:51 Oxygen tank no. 2 quantity Jumps to off-scale high and then begins to drop until the time of telemetry loss, indicating failed sensor. 55:54:52 Oxygen tank no. 2 temperature reads -151.3ø F. 55:54:52.703 Oxygen tank no. 2 temperature suddenly goes off scale low, indicating failed sensor. 55:54:52.763 Last telemetered pressure from oxygen tank no. 2 before telemetry loss is 995.7 psia. .... 55:54:56 Oxygen tank no. 2 pressure reads off-scale low fol- lowing telemetry recovery, indicating a broken supply line, a tank pressure below 19 psi, or a failed sensor. 55:54:56 Oxygen tank no. 1 pressure reads 781.9 psia and begins to drop steadily. 55:54:57 Oxygen tank no. 2 quantity reads off-scale high following telemetry recovery indicating failed sensor. .... 55:55:20 Crew reports, "I believe we've had a problem here." 55:55:35 Crew reports, "We've had a main B bus undervolt." 55:55:49 Oxygen tank no. 2 temperature begins steady drop lasting 59 seconds, probably indicating failed sensor. 55:56:10 Crew reports, "Okay right now, Houston. The voltage is looking good, and we had a pretty large bang associated with the caution and warning there. And as I recall, main B was the one that had had an amp spike on it once before." 55:56:38 Oxygen tank no. 2 quantity becomes erratic for 69 seconds before assuming an off-scale-low state, indicating failed sensor. 55:57:04 Crew reports, "That Jolt must have rocked the sensor on--see now--oxygen quantity 2. It was oscillating down around 20 to 60 percent. Now it's full-scale high again." .... __________ ~ CT |
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A13 O2 Tank Rupture Was Not An Explosion
It could more accurately be described as the cap getting blown off followed by O2 Ahh I think pressure relief valves would be a good addition to any tank. Keeping the pressure just below what would blow or permanetely damage the tank or systems. Plus vent them to prevent collateral damage in the event of a problem. The final vent port could be a burst one so as to defend from a bad or leaking valve. Was any of this added to later designs? If this would of been on apollo 13 the landing would of been scrapped but the crew would of had much of its oxygen and none of the fears of engine damage. That with the seperate battery and extra oxygen would of allowed a faster return and much less drama. Probably no movie. |
#8
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A13 O2 Tank Rupture Was Not An Explosion
It could more accurately be described as the cap getting blown off followed by O2 Ahh I think pressure relief valves would be a good addition to any tank. Keeping the pressure just below what would blow or permanetely damage the tank or systems. Plus vent them to prevent collateral damage in the event of a problem. The final vent port could be a burst one so as to defend from a bad or leaking valve. Was any of this added to later designs? If this would of been on apollo 13 the landing would of been scrapped but the crew would of had much of its oxygen and none of the fears of engine damage. That with the seperate battery and extra oxygen would of allowed a faster return and much less drama. Probably no movie. Forgot to add this isnt high tech, just check any hot water tank for at least the last 50 years or more. That pressure valve as saved lots of lives |
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A13 O2 Tank Rupture Was Not An Explosion
"Hallerb" wrote in message
... Nothing even vaguely resembling an answer to my question. If he simply "would of" posted an answer, I "would of" stopped reminding him. -- If you have had problems with Illinois Student Assistance Commission (ISAC), please contact shredder at bellsouth dot net. There may be a class-action lawsuit in the works. |
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