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#21
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Apollo service module question
Jochem Huhmann wrote:
Pat Flannery writes: Ah yes, the Russian ISS fans: http://www.newscientist.com/article/...s-hearing.html Yeah, I can very well imagine that noise is a major point of stress there. Probably much like living in string of server rooms with countless computer fans whirring all the time. I think I could stand that for a week or so but not much longer. Whenever I see a video from up there and listen to the audio I think "just like a long workday in the machine room, just without going home afterwards". No different than what we put up with on the boats, and it's not much better on surface craft. Didn't cause any stress. D. -- Touch-twice life. Eat. Drink. Laugh. http://derekl1963.livejournal.com/ -Resolved: To be more temperate in my postings. Oct 5th, 2004 JDL |
#22
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Apollo service module question
Pat Flannery wrote:
Jochem Huhmann wrote: Yeah, I can very well imagine that noise is a major point of stress there. Probably much like living in string of server rooms with countless computer fans whirring all the time. I think I could stand that for a week or so but not much longer. Whenever I see a video from up there and listen to the audio I think "just like a long workday in the machine room, just without going home afterwards". There's a distinct downside to it besides the hearing loss and annoyance factor also... all that noise is going to cover up sounds of other things that may be malfunctioning that you would want to shut down immediately if you could hear them. Not once you are used to the sounds around you. Been there, done that, and it wasn't a problem. D. -- Touch-twice life. Eat. Drink. Laugh. http://derekl1963.livejournal.com/ -Resolved: To be more temperate in my postings. Oct 5th, 2004 JDL |
#23
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Apollo service module question
Derek Lyons wrote:
Pat Flannery wrote: Derek Lyons wrote: We kept the hatches open because it prevented pressure differentials from building up and made atmosphere circulation easier. Did our sub's hatches have some way of equalizing pressure between two compartments after being closed and sealed? Yeah, but it wasn't very big. Well, I'm glad at least _we_ thought of that. Pat |
#24
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Apollo service module question
Derek Lyons wrote:
No different than what we put up with on the boats, and it's not much better on surface craft. Didn't cause any stress. The article spoke of permanent high frequency hearing loss on the Salyut and Mir crews...nothing you would want in regards to your sonarmen on a sub. Pat |
#25
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Apollo service module question
Dr.Smith wrote:
If memory serves correctly the engine bell was much larger then was needed for lunar docking method. Going along with this a think there may have been plans afoot to use actuators of some sort to extend and withdraw the bottom section of engine bell so as to allow for landing. Guess they got far enough along so they could not redesign engine/bell when they changed methods and so bell is a bit of fossil remnant from the direct ascent method.................Doc Sounds very unlikely to me. Once they'd chosen to use LOR they had to design and build a spacecraft (the LM) from scratch... and they didn't have time to shave some weight off the CSM? |
#26
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Apollo service module question
"Fevric J. Glandules" wrote:
Dr.Smith wrote: If memory serves correctly the engine bell was much larger then was needed for lunar docking method. Going along with this a think there may have been plans afoot to use actuators of some sort to extend and withdraw the bottom section of engine bell so as to allow for landing. Guess they got far enough along so they could not redesign engine/bell when they changed methods and so bell is a bit of fossil remnant from the direct ascent method.................Doc Sounds very unlikely to me. Once they'd chosen to use LOR they had to design and build a spacecraft (the LM) from scratch... and they didn't have time to shave some weight off the CSM? Keep in mind that a lot of things were going on in parallel. Once the SM design was fixed, it may not have been worth it to resdesign it. D. -- Touch-twice life. Eat. Drink. Laugh. http://derekl1963.livejournal.com/ -Resolved: To be more temperate in my postings. Oct 5th, 2004 JDL |
#27
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Apollo service module question
Fevric J. Glandules wrote:
Sounds very unlikely to me. Once they'd chosen to use LOR they had to design and build a spacecraft (the LM) from scratch... and they didn't have time to shave some weight off the CSM? Remember, the Service Module and its engine bell would have formed the _ascent_ stage of the lander in the direct ascent method. The landing stage was separate and far larger than the SM: http://www.brighthub.com/bh_controls...d=26808&page=1 Pat |
#28
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Apollo service module question
"Pat Flannery" wrote in message dakotatelephone... Fevric J. Glandules wrote: Sounds very unlikely to me. Once they'd chosen to use LOR they had to design and build a spacecraft (the LM) from scratch... and they didn't have time to shave some weight off the CSM? Remember, the Service Module and its engine bell would have formed the _ascent_ stage of the lander in the direct ascent method. The landing stage was separate and far larger than the SM: http://www.brighthub.com/bh_controls...d=26808&page=1 Yea, the landing stage for the direct method was absolutely freaking huge. That's why direct would have required the Nova launcher. It would have made Saturn V look small by comparison. Jeff -- "Take heart amid the deepening gloom that your dog is finally getting enough cheese" - Deteriorata - National Lampoon |
#29
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Apollo service module question
Jeff Findley wrote:
Yea, the landing stage for the direct method was absolutely freaking huge. I once remember it being described as like trying to land a Atlas ICBM tail-first. The Soviet direct ascent lander was a lot smaller: http://www.novosti-kosmonavtiki.ru/c...s/200/36.shtml It used a separate stage to brake it into and out of lunar orbit, which was jettisoned before landing: http://www.astronautix.com/craft/lk700.htm Pat |
#30
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Apollo service module question
Derek Lyons wrote:
"Fevric J. Glandules" wrote: Sounds very unlikely to me. Once they'd chosen to use LOR they had to design and build a spacecraft (the LM) from scratch... and they didn't have time to shave some weight off the CSM? Keep in mind that a lot of things were going on in parallel. Once the SM design was fixed, it may not have been worth it to resdesign it. Big lump of metal like an engine bell? Sorry, not buying it. They had time, and motivation. |
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