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Correct, the CM was sandwiched between the LM and the SM. This means that the LM was shielding the CM from any particles approaching from the front and the SM was protecting the astronauts from behind. This means that only particles approaching from the sides would need to be shielded by the CM alone.
Originally posted by backinblack
reply to post by DJW001
Correct, the CM was sandwiched between the LM and the SM. This means that the LM was shielding the CM from any particles approaching from the front and the SM was protecting the astronauts from behind. This means that only particles approaching from the sides would need to be shielded by the CM alone.
But wasn't the LM actually BEHIND the CM at launch and was only docked to the front later?
A task that would take quite some time while both were still within the VAB I presume??
Originally posted by FoosM
Originally posted by backinblack
reply to post by DJW001
Correct, the CM was sandwiched between the LM and the SM. This means that the LM was shielding the CM from any particles approaching from the front and the SM was protecting the astronauts from behind. This means that only particles approaching from the sides would need to be shielded by the CM alone.
But wasn't the LM actually BEHIND the CM at launch and was only docked to the front later?
A task that would take quite some time while both were still within the VAB I presume??
Saying that the LM and SM shielded the CM, is like trying to use an umbrella underwater.
Sure one side had more protection, that wasn't the issue raised. We are talking about the fact that the CM was not surrounded by the same amount of material as NASA pretends it was. Many parts were alot less thick than others. Still though, the radiation was not an issue. So either the radiation was not a problem, or the CM, no matter how thin the craft was, was still more than sufficient to block it. Either way, it should mean that longer missions to the moon should be very easy to do.
Have you noticed that nobody really has come up with an answer backed by facts?
I simply posed the question, how much longer could Apollo actually stay on the moon?
I would think that an Apollo supporter would jump at the chance to prove hoaxers wrong with this information.
Originally posted by Reaper2137
Originally posted by FoosM
Have you noticed that nobody really has come up with an answer backed by facts?
I simply posed the question, how much longer could Apollo actually stay on the moon?
I would think that an Apollo supporter would jump at the chance to prove hoaxers wrong with this information.
Well it is based on the size of the craft foosm a craft that small could only carry so much,
Both programs turned into a waste at the end if you ask me. So much more could have been done, just no one cared..
However, for outpost missions to the moon lasting about 180 days or Mars missions expected to last from 600-1000 days, effective doses from GCR will be much higher (Table-5) than past space missions because of the absence of the magnetic protection provided by the Earth from lower energy GCR components and longer duration of the missions. In addition, a significant probability would exist for one or more large solar particle events.
Originally posted by Aloysius the Gaul
Does this document cover all the required points about long tern radiation exposure?
However, for outpost missions to the moon lasting about 180 days or Mars missions expected to last from 600-1000 days, effective doses from GCR will be much higher (Table-5) than past space missions because of the absence of the magnetic protection provided by the Earth from lower energy GCR components and longer duration of the missions. In addition, a significant probability would exist for one or more large solar particle events.
I posted it before, but I haven't seen any comments on it directly.....
past space missions because of the absence of the magnetic protection provided by the Earth
Originally posted by Reaper2137
But if I had to guess man, I would say that if they only got enough radiation from lets say like 2-4 X-Rays a day than I would think that they could safely stay up there for a year or two before they would have to be treated..
Originally posted by FoosM
Originally posted by Aloysius the Gaul
Does this document cover all the required points about long tern radiation exposure?
Are you asking because you are not sure what the document is saying, or do you think that the document does answer the questions that were asked? If so, can you quote the relevant parts we should read? Because I dont see where it answers my question of how long Apollo could of technically stayed on the moon if radiation was the only consideration.
However, for outpost missions to the moon lasting about 180 days or Mars missions expected to last from 600-1000 days, effective doses from GCR will be much higher (Table-5) than past space missions because of the absence of the magnetic protection provided by the Earth from lower energy GCR components and longer duration of the missions. In addition, a significant probability would exist for one or more large solar particle events.
I posted it before, but I haven't seen any comments on it directly.....
past space missions because of the absence of the magnetic protection provided by the Earth
Why would they say this, and not use Apollo as an example? Or as a benchmark?
Originally posted by Aloysius the Gaul
Originally posted by FoosM
Why would they say this, and not use Apollo as an example? Or as a benchmark?
Apollo exposure IS given in there - along with other missions - Mercury, Gemini, Skylab & others.
The point is that you claimed that NASA has not addressed the "killer flares". You have provided no evidence of this. You have not even admitted you were wrong.
Originally posted by FoosM
Originally posted by 000063
Tell you what, I'll do my best look up the information you're asking for right after you produce the "killer" solar flare/SPE numbers to support your claim. I can't guarantee I'll find it, but I'll do my best.
I mean, I looked up what evidence there was of solar flares presented in this thread, and I found you making a similar claim that "major" flares/SPEs occurred. When asked what was "major", you said you were using NASA's definition. When asked what that definition was, you asked the debunkers what NASA's definition was, and changed the subject in the usual fashion.edit on 2011/7/22 by 000063 because: /
Well whats the point? If Apollo could withstand major solar flares, then it really doesnt matter which flares I mention.
Because you are exposed to more radiation the longer you are in space.
So its quite clear that Apollo's aluminum hull, would have sufficiently protected the astronauts from even a massive "killer" flare. And obviously they dont have to go to the moon during Solar Max, they can go during Solar Min. What is the excuse for NASA not returning to the moon for longer missions or Mars? Why are they saying the issue is radiation?
Originally posted by 000063
Go outside on a sunny day. Sunlight has UV radiation. If you go outside for short periods, you become pale (assuming you're white). Go outside a moderate amount, and you get a healthy skin tone. Too much, and you get sunburns and skin cancer.
Similarly, months in space would mean more exposure to radiation than a few days in space. I cannot explain it in any simpler terms.
Originally posted by FoosM
Humans can withstand a single exposure of 25 rads of (Hard Xrays or Gamma Rays)
20 rads may cause Nausea.
100 will induce vomiting.
200 your temporarily sterile.
500 your sterile and you will die in a few months.
1000 and above, your dead.
Cosmic Rays - 10 mrads a day
Inner Belt - 100 rads an hour
Outer Belt - 10,000 rads an hour
The inner belts is composed of two types of energetic protons and electrons.
Now what about the protons in the belt? They consist of several hundred MeV. Which is equivalent to low energy solar flares. You need about 1.5 inches of aluminum to bring them down to 4 rads an hour. You need 3 inches of aluminum to reduce it to 2.2 rads an hour.
The Apollo CM.
The craft NASA states have carried astros to the moon and back.
The thickness of the outer wall, made from stainless steel brazed honeycomb between steel alloy face sheets, varied from 0.5-inch (1.27cm) to 2.5-inch (6.35cm). Now mind you, this is for thermal radiation. Not shielding for ionized radiation. Though anything between you and radiation is a good thing.
0.75 + 0.5 = 1.25 cm worth of various material. Which is not the same as 1.5 inches of pure aluminum, because a lot of it is HONEYCOMBED. It had air inside! Thats the so called shielding of the CM. Now either thats sounds like they planned to cross the atlantic with a small fisherman's boat. Or the ocean was actually a small lake.
So this ship would be getting for sure its dose of at least 4 rads an hour of energetic protons via the thinnest section of the hull. Conservative estimates the trip to be 90 minutes to and 90 fro. Thats three hours (3 x 4 = 12 rads). Other estimates vary from 3 hours to and 3 hours fro (3 x 9 = 27 rads). I've even seen estimates of the trip taking seven hours (3 x 14 = 42 rads).
The highest dose received from the missions was like 1 rad and change. Does this make sense?
Now what about the electrons?
You can stop electrons with a few millimeters of aluminum, however, once you do, bremsstrahlung occurs.
-And this is why you need to use LEAD. Because aluminum, will start to create several rads of soft-xrays an hour !
In some cases, e.g. 32P, the bremsstrahlung produced by shielding the beta radiation with the normally used dense materials (e.g. lead) is itself dangerous; in such cases, shielding must be accomplished with low density materials, e.g. Plexiglass (lucite), plastic, wood, or water;[10] because the rate of deceleration of the electron is slower, the radiation given off has a longer wavelength and is therefore less penetrating.
Originally posted by DJW001
reply to post by FoosM
Now what about the electrons?
You can stop electrons with a few millimeters of aluminum, however, once you do, bremsstrahlung occurs.
-And this is why you need to use LEAD. Because aluminum, will start to create several rads of soft-xrays an hour !
Wrong. The denser the material, the greater the bremsstrahlung. It has to do with the nuclear weight of the atom.
In some cases, e.g. 32P, the bremsstrahlung produced by shielding the beta radiation with the normally used dense materials (e.g. lead) is itself dangerous; in such cases, shielding must be accomplished with low density materials, e.g. Plexiglass (lucite), plastic, wood, or water;[10] because the rate of deceleration of the electron is slower, the radiation given off has a longer wavelength and is therefore less penetrating.
en.wikipedia.org...
Originally posted by FoosM
Originally posted by ConspiracyNut23
reply to post by FoosM
I think they are worried about the galactic cosmic ray exposure, not exposure to solar flare.
Well which one is it, because Im seeing reports for either or.
I dont understand why after 40 years, including the success of Apollo, this is not clearly
agreed upon in the scientific community. There must be a scam going on.
Corporations using scientists to milk unnecessary research money from the Government.
Originally posted by FoosM
[long post deleted by moi ... see it above]
The highest dose received from the missions was like 1 rad and change. Does this make sense?