It looks like you're using an Ad Blocker.
Please white-list or disable AboveTopSecret.com in your ad-blocking tool.
Thank you.
Some features of ATS will be disabled while you continue to use an ad-blocker.
NASA has just announced the shuttles successor and the possibility of manned deep space missions
Originally posted by playswithmachines
reply to post by Frira
There you have it, then;
Except for the Apollo missions to the Moon, NASA's manned spaceflight missions have taken place within the cocoon of the Earth's magnetosphere. Between the Apollo 16 and 17 missions, one of the largest solar proton events ever recorded occurred, and it produced radiation levels of sufficient energy for the astronauts outside of the Earth's magnetosphere to absorb lethal doses within 10 hours after the start of the event. It is indeed fortunate that the timing of this event did not coincide with one of the Apollo missions. As NASA ponders the feasibility of sending manned spaceflight missions back to the Moon or to other planets, radiation protection for crew members remains one of the key technological issues which must be resolved.
Not so safe, after all
From the Newscientist;
...would depend on the destination, which is not yet clear, although President Obama has called on NASA to send astronauts to visit an asteroid by 2025.
Don't worry, by that time a few asteroids will have visited US.....'edit on 18-9-2011 by playswithmachines because: Add info
Originally posted by Ilyich
reply to post by Frira
So would that mean that the estimated exposure to radiation through the VAB both ways would total approximately 3 ?
Now, don't take me wrong here, this is obviously passing through the safest or in other words the thinnest point of the VAB ? Now, most Diagrams of the VAB show that it's Earth's Magnetosphere that has " Trapped " Gamma, solar, and other galactic radiation correct ? Not the entire magnetosphere but it seems to play a very significant role in it's mean. Okay, so here's my question, wouldn't this put the safest trajectory either straight out Earth's magnetic poles, or very near to them ? Wouldn't this in fact be the least favourable path to the moon ? Again, I'm stating my question based on what I already know, as well with out looking up significant information in regards to shuttle launch positions, or the lunar position at the time of the launch as well as the calculated point of interception. Now I would imagine the ideal trajectory would be planned to minimize radiation exposure, limit the use of fuel to get to the moon, and match it's speed to then enter it's orbit. So the rest of the mission can be carried out.
So if this is the case the moon would have to be in a position to provide sufficient time to navigate the VAB safely, then either slow down to match the lunar orbit, or accelerate to " Catch Up " to the moon as it makes it's pass.
...
Basically the Apollo Rockets were built in a way that each progressive step, or vehicle was disposable right ? Now as far as the orbiter goes, as well as the lander and return vehicles, based on the limitations of the time, weight was a very considerable obstacle. ...
...
They state they basically only had enough to go to the moon and return to a point the pod ( Return vehicle ? ) could re-enter Earth's Atmosphere. I don't want to look up details as this was meant to be quick but I'm getting way into this. If they got off course, wouldn't they have to take the quickest path home ? ...
Originally posted by butcherguy
But our (the U.S.) current 'manned' space program is the X-37 B. X usually stands for experimental. It is the Air Forces' toy though not a NASA project that will be dropping off suitcases at the ISS.
Originally posted by WorldObserver
... and be capable of launching humans beyond low Earth orbit
which proves that they have NEVER been beyond Low Earth Orbit! So, no moon landings finally admitted!
Originally posted by Ilyich
reply to post by Frira
How could a Lunar return vehicle exit lunar orbit safely, at a point that would provide the best trajectory towards one of the poles ?
However, the outbound and inbound trajectories of the Apollo spacecraft cut through the outer portions of the inner belt and because of their high speed spent only about 15 minutes in traversing the region and less than 2 hours in traversing the much less penetrating radiation in the outer radiation belt. The resulting radiation exposure for the round trip was less than 1% of a fatal dosage – a very minor risk among the far greater other risks of such flights. I made such estimates in the early 1960s and so informed NASA engineers who were planning the Apollo flights. These estimates are still reliable.
...How much fuel could it really contain being it's the last step, in the progressive vehicle or rocket ? I don't expect you to know, but if you do can you help me out here ?
This is all an amazing feet of science, that obviously took countless hours of planning and many trials and failures to achieve. A lot of these areas confuse me, as well leave me reeling and open for plenty of dis-info to be implanted. I don't often get a chance to talk to people of a caliber suited for these questions. If I need to I will state the sources that lead to my quest