I just had a read of Chris' latest article...
John, did we read the same article?
Holy reading comprehension skills, Batman!
[The SEV] is probably the "lander" that is thought to be "cheaper"
I saw no talk of a lander.
That's correct, the article does not talk of a NEO lander. "In the continual debate on this forum", the idea of a lunar lander is compared to a roughly equivalent NEO lander, with the former being characterized as too expensive, due to its need to escape Luna's gravity well. The roughly equivalent NEO lander, won't have this showstopping requirement. Left unsaid in the "continual debate", of which this thread is a part, is a comparison of the two missions and their total costs and values. Left unsaid in your response is any opinion of yours regarding this comparison, leaving me to believe that you are in favor of
"Asteroid Next" missions. These missions should not be a goal of NASA's at all at this time, in my opinion.
From the article, I took this
picture to be the SEV; the picture was uncaptioned, and I took the adjacent text to refer to it. So I can certainly be accused of web laziness regarding my research of that picture.
Such a craft would probably offer a shirtsleeve environment for the astros to pick at the rock...
Then you start wildly postulating super-expensive sounding capabilities for your fantasy of the SEV "lander" like allowing "astros" to touch the asteroid without a spacesuit on.
(This [the SEV] is a) modular vehicle that combines a pressurized cabin and crew support equipment, a propulsion/consumables unit, and robotic support packages...
I hope I'm not "wildly postulating" that a "pressurized cabin" would allow the astros to work in a "shirtsleeve environment". I would also hope they would keep the airlock closed while they peck around on the rock, tho. That way, they wouldn't have to keep their space suits on while in the pressurized cabin. But hey. In addition, you are certainly free to believe that the article's postulated capabilities of the spacecraft are
not "super-expensive sounding capabilities". And while I am totally in favor of an SEV in principle, I am sure that it will be an expensive vehicle to develop.
It is not a lander, and most all of its components are just versions of hardware currently in use. Your point about it being just as hard/expensive to develop as a lunar lander is hard to understand.
That "most of" the SEV's components are "currently in use" is an assertion that I would not make, and that you cannot defend.
But John's proposing a lunar base for four astros, what about all that infrastructure?
And don't get me started with your level playing field logic: You claim an equal budget comparison, but your NEA mission only manages to go somewhere with a negligible gravity well and brings back some samples, while the moon mission starts building a city on the moon and some how you think these things will cost the same?
The ISS has six folks on board, so I suppose that "city" is 50% larger than the uhhh, "city", I suggest. "A level playing field would suggest trading the two missions with the same budget and the same duration: 500 days, and put a valuation on..." the results from either mission. And the same mass, I forgot to add. True, I make light of the expected return from a NEO mission, but I do present a short list of their probable accomplishments, and compare that list with the probable accomplishments of four astros on the Moon. There is no official side by side comparison of the two possible missions that I describe.
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one of the things that is continually missed in the ongoing debate about the utility of a NEO mission is the mission duration. Here, the astros would spend a week at the NEO and 243 days in transit, running the treadmill and playing video games. For a lunar mission, they'd spend a week in transit and 243 days on the surface, doing field work. Dollar for dollar, you're going to get more work on Luna. And more value.