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A 500 footer asteroid sounds more feasible and glad you're being realistic there, but I doubt the realism for a mass driver for two reasons:
1) One's never been built or used, certainly not in space and not on Earth.
2) Most asteroids are not heavy metals, and likewise material not magnetic.
Those are the achilles heal of the much-vaunted mass driver.
Still not a bad idea, the NEO...at least to a degree. It'd be an extensive project and, for safety and international reasons, likely require 30 years to organize and then implement. Ares tech might be able to do it if a stradegy can loft several boosters to the asteroid.
One last problem...after all this effort...what are we going to use this asteroid for? Strike out the Phobos-referenced-fuel idea...our neighboring NEOs are virtually all stony: little metal and no carbon-water resources.
Whatever purpose it'd serve...I wouldn't recommend putting it any closer than geosyncronus - lord forbid a terrorist gaining control of the asteroid's nagivation systems...
I can't seem to load the massive PDF but what you posted looks interesting cyclops. So this is info on the first Orion test right?
I remember how the ol' LEM was occassionally referred to as a "bug"
Looking at how damn BIG Altair, formerly known as LSAM ....
I have to say that's a pretty big bug alright.
The new images look impressive - it'll be interesting to see how they compare when Altair becomes reality.
Something occured to me when I recalled the discussion about common bulkheads being more of a problem. Considering there's a few hundred degree difference between the liquid point of hydrogen and liquid oxygen I see, and no doubt the engineering is tricky too but also no doubt insulation is a major factor between the two cryogenics...
...but what about common bulkheads between liquid oxygen and methane? The two are fairly close, or at least closer than that of hydrogen and oxygen; would this make bulkheads in a LOX/CH4 system easier to deal with? If so then it might mean Martian vehicles (and perhaps future Lunar ones) have one advantage in design.
I have to admit the Merridiani sites look very plain if the map topography is any indication; like Opportunity MSL might luck out on finding something.
Personally I hope for one of the Vallis sites; there should be both mineral evidence as well as something to look at either.
I seem to recall in his "Mars Direct" book that, regarding the exact same topic, he pointed out how even a jet trying to rendevous with this thing would be suicide - how the HELL do you latch onto something moving a couple hundred miles an hour faster than you without sheer luck and survive...in less than a dozen pieces? :shock:
Couple of additional sections worth quoting from that same document:
• Both NTO/MMH and LOX/CH4 under consideration
• Initial LDAC-1 design assumed NTO/MMH integrated RCS/MPS
• After completion of LDAC-1, Ascent Propulsion System redesigned
using LOC/CH4
...and then
• Design
– LO2 and Methane are loaded subcooled and allowed to
absorb heat leak and warm over the LEO loiter, transit, and
210 day surface stay
• Thermal Modeling Has been performed by GRC and
MSFC to validate this approach
– Both models show heat leaks that result in zero boil-off for
the outpost mission
– Sortie Mission capability for zero boil-off also exists
It's great to find this positive research and thinking on Methane engines. And yeah, that 210 day stay on Lunar surface is ANOTHER step in right direction for Martian vehicles. If you can make a vehicle that can store cryogenic fuel in an enviorment that fluxes temperature nearly 500 degrees over the course of a month...I think that can probably do the same job at Mars (while cold, you have to admit it's alot more STABLE temperature-wise than the Moon).
Anti-Moon bloogers, grab a plate and start eating your hearts out 'cause there's no way this same tech for Mars would be developed...before 2050 and you guys are preparing to retire.
The Vision is moving in the right direction 8)
Simply spectacular. 8) They have less reason to call a methane engine "experimental" anymore now.
I think all of you are right about all of these things.
Altair will give us the best chance to make a salvageable vehicle since it's going to have cargo capability. Also, considering the Apollo 13 astronauts were able to use a square filter from the LEM for the round ones in the CM...even if it's not a perfect fit it shows you the engineers will find a way around a problem. 8)
Commadore...yeah, good chance we'll have to bring more hardware but still won't hurt to try, especially if we want to be simultainiously exploring, cost-cutting, and realistic.
Not a bad choice and complements' the "A"-theme with Ares. The Eagle reference is a nice bit of heritage since it's well-associated with Apollo 11 now.
I consider Congress the more finicy element as opposed to the J-2X, especially with elections coming up.
I think it is admirable that Griffen and NASA are doing their best when what they've got
An excellent idea to try at the moon. Hopefully they can attempt this at Mars and Venus, especially the later since we still aren't sure on Venus' development.
I'm not exactly thrilled about this:
If Congress fund it and take responsibility for the risk of continuing to fly, it's one solution. NASA have said it will cost about an extra $3 billion a year to keep Shuttle flying to provide crew access to ISS, so that will be about $12 billion more until Orion is ready. The minimum would be about two flights a year to provide crew access to ISS, that's an expensive ride.
It would be, and I wouldn't suggest for them to fly anymore than that. Hell if they fly the shuttle may as well bring the crew roster up to 4 if not six while it's running.
I'm not exactly thrilled about this:
Okay after doing some research here is the design for the Pilyhas -1 the first inter-lunal vehicle that could travel to the moon deliver crew and cargo and then re-turn to the ISS, be broken down into modules for storage and re-assembled for trips back to the moon.
Two problems with relying on the ISS:
1) The ISS has only a handful of docking ports, most Russian, and the Russians have been boasting lately about planning to expand their portion of the ISS - they likely would refuse using any port for the docking of non-Russian hardware. Beyond any of these ports there aren't really any dedicated latches or spots on the truss for 'stowage' that wouldn't interfer with either the radiators or solar panels in some way. :?
2) Very lousy orbit for Lunar travel. It'll cost more fuel launching from the 52 degree inclined orbit that just directly from whatever launch site. The Moon orbits...what, 2 or 3 degrees off our equator? Whatever CEVs flying to the ISS will be optomized for nothing but that.
A reuseable Service Module would be a great idea though, and although I'm against space stations whenever possible a station that actually acts as a stowage yard might not be bad - but still if the SM can orbit on its own let it do so w/o a station to play den mother.
Their going to take these sensors off on Ares V right?
There should be an override for this. We know how much fuel there is, faulty sensor be dammed.
Agreed wholeheartedly. I don't recall unmanned rockets being scrubbed as often...
Whatever screws up the STS' ET and SRBs they ought to examine thouroughly and amend if they use both as a base for Ares V...and to an engineer both simplifying and improving tend to fall into the job description.
That's depressing.
To anyone still advocating the shuttle can be 'reused' for another 10 years I blatantly throw this launch delay in their faces: they had remarkably good weather and the ESA staff gathered in support only to have a 4 devices out of a machine loaded with thousands ruin it all.
It's never good depending on a vehicle this finicky. Even if ANOTHER three years is needed to develop the Ares & Orion I'll WAIT them out willingly and still give my tax payer dollars in support of it...
...and I'm talking to YOU gaetomon on that last remark. 8)
Mars orbit. MArs Direct is not really equipped for exploiting Phobos, so some varient of the Design reference mission should be used. I also think a regolith mining operation might require the full attention of 6 astronauts, at least until we can work out the bugs of the thing and get robots to do it.
To visit not-so-much; I mentioned earlier that all you really need is just a CEV and a tether - no dedicated lander nessicary although if they chose to develop one for NEOs the Martian moons would be applicable for it as well.
To exploit long-term...yes, some extra hardware likely needed. Thinking about it though, an initial outpost doesn't nessicarily have to be sitting or embedded in the moon - it could be tethered just like the CEV idea. That gives more ideas...how to EXPLOIT the moon despite the weightlessness:
A tethered station doesn't nessicarily have to remain in the same spot. Just hook up a new tether a little ways away, disconnect the old and reel the station to new spot. Assuming the Martian moons are meters-thick coated with fluffy dust...to exploit w/o the hastle of mounting equiptment to rock or losing it in the dust apply something like a vaccum cleaner - yes I know ridiculous in the vaccum of space but it could use say a small gas jet to funnel the dust for instance. Once enough of a spot on the moon is sucked up just pull the station along kinda like a balloon.
How does that sound? Argue about how to the suck-up the dust but a tether setup is fairly straight-forward. If the tether comes loose it's not like the station's going to fly away - it'd already be flying in rendevous with the moon.
Great view - hopefully Columbus' hook-up with go as smoothly.
MEX got much closer to Phobos a while ago and has also been doing spectroscopic analysis. Indications are that it is a carbonaceous chondrite asteroid.
I'm curious to know if any of these spectroscopic readings suggest if the Martian moons have exploitable resources.
It will be interesting to learn what MRO's sensitive intrument can tell us about the properties of the Martian moons. Given CRISM detected plenty of water-bearing minerals on Mars already it has a fair chance to do the same for the moons.
These CRISM measurements are the first spectral measurements to resolve the disk of Deimos, and the first of this part of Phobos to cover the full wavelength range needed to assess the presence of iron-, water-, and carbon-containing minerals.
Where is that damage located? I'm guessing space junk strike since it looks like shotgun holes.
I sincerely hope some of these will pan out. So far only Bigelow has proven to be competent enough to handle space flight and being more than just a one-hit-wonder at it, but obviously we need a vehicle that can shuttle down to Earth.
Hopefully COTS won't prove to be NASA's bane but at least there' potential.
That sounds like fantastic news cIclops - with these results NASA might finally look toward LOX/Methane as the ideal propellant.
For now, obviuously, it'd be limited to LSAM's ascent stage but that sounds like a perfect test application. Future variants or successors to Orion might very well utilize the same technology too, especially when Mars missions become a real possibility.
Don't hold your breath over it; rockets use the stuff ALOT more than cars so guess where demand will be? 8)