They won't need that much water. Even 10km³ will go a long way. Since that much water is in many locations they can look for other criteria.
Quote from: guckyfan on 11/23/2016 12:04 pmThey won't need that much water. Even 10km³ will go a long way. Since that much water is in many locations they can look for other criteria.But we're talking about the vision of building a city, and of sending a million colonists to live and work there. Even if the colony recycles water efficiently, there's still going to be a lot of spaceships departing for Earth (since their recyclability is key to the whole plan), and those will be needing a lot of water collectively.The Mars settlement will be a spaceport in its own right - at least over the long run - and thus you'll want to have abundantly ample resources available for scaling over the long term.
Large deposit of water ice the size of Lake Superior found just under the martian surface at Utopia Planitia:Why not simply go where the water is?
Otherwise, what other possible criteria would be important for selection of landing site and location of settlements?And the place has got one other plus - since Musk is a notorious sci-fi nerd, I'm sure he knows (as the rest of us do) that Utopia Planitia is the location of the shipyard where the USS Enterprise is built in the 24th century, in the Star Trek story universe.I'm sure he wouldn't pass up mentioning that, if this place met all his other criteria for a suitable spot.
Quote from: sanman on 11/23/2016 11:27 amLarge deposit of water ice the size of Lake Superior found just under the martian surface at Utopia Planitia:Why not simply go where the water is? Well the main disadvantage of Utopia Planitia is it is very, very, very boring. Viking 2 landed in the closest thing to what was Utopia's more interesting terrain, with the crater Mie to the east and Hrad Vallis to the south. I glanced at a map of the coordinates - there are a few ruples features and a spattering of small, unnamed craters...but literally nothing on the scale of tens, if not hundreds, if kilometers. Aside from a bland landscape, the science may be minimal outside of deep drills.I think a big reason why Utopia Planitia is such a boring place is, in the ancient wet days of Mars, it was Mars' equivalent of Earth's abyssal plains under the ocean. These regions technically dominate huge chunks of the Earth's surface, and by dominate I'm talking on the scale of continents since they are legitimately a full HALF of Earth's true surface (certainly if you talk to any oceanographers). Utopia is basically a fossilized version of these massive mud flats.Quote from: sanman on 11/23/2016 11:27 amOtherwise, what other possible criteria would be important for selection of landing site and location of settlements?And the place has got one other plus - since Musk is a notorious sci-fi nerd, I'm sure he knows (as the rest of us do) that Utopia Planitia is the location of the shipyard where the USS Enterprise is built in the 24th century, in the Star Trek story universe.I'm sure he wouldn't pass up mentioning that, if this place met all his other criteria for a suitable spot. Science and safety are the essential criteria. I'd personally rank a flat spot adjacent to Valles Marineris the best. However, I would put Utopia as my second choice now since it is generally safe and ice rich. My only additional requirement would be some form of long-range transport for a Utopia base to expedite exploration.I don't know what Musk's perference would be on where to setup a Mars base for ITS. Utopia might be fitting, but given his choice of "Heart of Gold" he may favor more British-themed locales bear-in-mind.
Musks presentations always show the red mars turning blue. Perhaps elevation should also be considered a significant factor in selecting the first landing site. Somewhere above global sea level if the planet were terraformed and somewhere not likely to become a lake or other inland body of water but perhaps next to a future place like this.
Posted it here before but since this is another thread on manned landing sites...NASA survey of potential landing sites...https://www.nasa.gov/sites/default/files/atoms/files/exploration-zone-map-v10.pdfN.B. Nili Fossae is the closest to this Lake Superior glacial ice in Utopia Plantina
The predicted typicalmean annual surface temperature for the EZ investigatedlatitudes is -60ºC [5]. At these temperatures,permafrost could have a mechanicalstrength close to that of limestone [6, 7], whichcould have stabilized evacuated caverns. Chemicalprecipitation from circulating brines in terrestrialcold springs can produce cements along theperiphery of feeder conduits, thereby enhancingtheir overall structural stability [8]. Cements developedin association with cold water circulationinclude calcite, aragonite, Fe-Mn oxides, sulfidesand sulfates [9,10]. On Earth, caverns are knownto occur in ice-welded sediments such as in associationwith networks of ice wedges in permafrost[11] and ice-welded moraine deposits [12]. Someglacier caverns are known to have remained stableover decades [13]. Subsurface caverns andsteep walls in Hebrus Valles might represent naturalterrain features that can be adapted for constructionpurposes (minimum ROI requirement).,Hence, infrastructure can be emplaced or constructedthe LS (minimum ROI requirement).
a little far north for best solar
Quote from: philw1776 on 11/27/2016 02:45 pma little far north for best solarCorrect in regards to Utopia overall. The Hebrus Valles site I mentioned is more southerly but likewise farther from direct ice deposits. Also, given we're talking about SpaceX's plans, in the end they may not choose a site NASA scientists advocate simply because they might favor engineering concerns more heavily than science (such as the need for solar power).
Quote from: redliox on 11/27/2016 03:46 pmQuote from: philw1776 on 11/27/2016 02:45 pma little far north for best solarCorrect in regards to Utopia overall. The Hebrus Valles site I mentioned is more southerly but likewise farther from direct ice deposits. Also, given we're talking about SpaceX's plans, in the end they may not choose a site NASA scientists advocate simply because they might favor engineering concerns more heavily than science (such as the need for solar power).For colonization, engineering concerns are more important than scientific research. Once the initial base for the colony is established, explorers can drive rovers to more interesting sites for science.The key is to build a colony that will eventually become self-sufficient. Once the "beachhead" on Mars is established, other benefits such as science and multi-planet species will naturally follow.Access to water is the most important ISRU factor. Utopia Plantina sounds to me like a good place to start.
Quote from: wes_wilson on 11/26/2016 12:18 pmMusks presentations always show the red mars turning blue. Perhaps elevation should also be considered a significant factor in selecting the first landing site. Somewhere above global sea level if the planet were terraformed and somewhere not likely to become a lake or other inland body of water but perhaps next to a future place like this.The time scale between establishing a first colony and eventual filling of lakes or oceans via terraforming (if ever) will make it a non-issue. If the best place for initial colonies happens to be an area that gets flooded 1000 years from now so be it, they can build on higher ground later.Or do you think they can produce standing water in a lake 50 years from now? I don't think so.
The timeline for terraforming is probably best for another thread. However, my view is that it could be much shorter term than most people think. On earth, we've already warmed the planet several degrees over the last 150 years as a byproduct of our society. A focused industrial effort to produce super greenhouse gases could effect more rapid change on a shorter timescale. Further, Mars doesn't have the same strong feedback mechanisms in place to prevent climate change. A little warming will release a lot of CO2. A breathable, stable oxygen atmosphere without unacceptable toxin levels, strong magnetic field and a biosphere is a whole different basket of eggs - but temperature and liquid water isn't.So, I think elevation is a factor if you're planning for long term inhabitation of Mars.
Quote from: wes_wilson on 11/28/2016 11:10 amThe timeline for terraforming is probably best for another thread. However, my view is that it could be much shorter term than most people think. On earth, we've already warmed the planet several degrees over the last 150 years as a byproduct of our society. A focused industrial effort to produce super greenhouse gases could effect more rapid change on a shorter timescale. Further, Mars doesn't have the same strong feedback mechanisms in place to prevent climate change. A little warming will release a lot of CO2. A breathable, stable oxygen atmosphere without unacceptable toxin levels, strong magnetic field and a biosphere is a whole different basket of eggs - but temperature and liquid water isn't.So, I think elevation is a factor if you're planning for long term inhabitation of Mars. Agreed. Whilst it probably doesn't matter if initial work is low level, there's no genuine reason why it needs to take a thousand years to significantly raise the temperature (a thousand years is the time between the early middle ages and the present day, think of the technology climb in that time. We will likely have a technology development rate in the near future which exceeds what we learnt in 1000 years in 100, 50, or less, and it will just keep on climbing. With present day tech it hypothetically doesn't need a thousand years, with unknowable future tech? Assume better ratios under optimistic, Muskian colonisation scenarios).There's a lot of satisfactory mid-ground or higher ground sites that it's unlikely to be a problem anyway.
My guesses at SpaceX site criteria0. Low enough below mean datum for sufficient aerobraking for landing (-2Km or lower) & low enough latitude (under ~30 degrees) to minimize landing & takeoff delta V. Excess landing deltaV makes colony $/ton landed freight bill more expensive. More trips/thousand tons. Excess takeoff deltaV consumes more energy intensive ISRU resources.1. ISRU: water available in colony need quantities2. ISRU: solar power available in colony quantities as mining water and especially disassociation eats electrons3. Given 1&2 sufficient water & solar power available for colony4. Other ISRU needs: minerals etc. for colonial development5. Interesting site & nearby attractions that motivate large #s of folks years to a lifetime off planetMusk is a marketeer; looking cool is important to selling the dream & human satisfactionNASA Priorities:0: ~ same as SpaceX 1. Sufficient ISRU to support small base camp for a synod & return propellant2. Science: geological history of Mars3. Science search for evidence of past life4. Science search for existing life. Base away from but accessible from search site accessed by tele-operated sterilized planetary protection rover
For colonization, engineering concerns are more important than scientific research. Once the initial base for the colony is established, explorers can drive rovers to more interesting sites for science.The key is to build a colony that will eventually become self-sufficient. Once the "beachhead" on Mars is established, other benefits such as science and multi-planet species will naturally follow..
Utopia Planitia may be boring BUT it has a basically unlimited water supply. IMO, the ideal place to set up the solar and ISRU plants needed. Plenty of area to build an initial base to establish a foothold. Plenty of room to locate landing zones far enough away from other structures. So what if you have to drive 10klm from the ITS to the base. It's not hard with the right vehicles.Land, get set up safe and comfortable and then worry about science and exploration.
My guesses at SpaceX site criteria0. Low enough below mean datum for sufficient aerobraking for landing (-2Km or lower) & low enough latitude (under ~30 degrees) to minimize landing & takeoff delta V. Excess landing deltaV makes colony $/ton landed freight bill more expensive. More trips/thousand tons. Excess takeoff deltaV consumes more energy intensive ISRU resources.1. ISRU: water available in colony need quantities2. ISRU: solar power available in colony quantities as mining water and especially disassociation eats electrons3. Given 1&2 sufficient water & solar power available for colony4. Other ISRU needs: minerals etc. for colonial development5. Interesting site & nearby attractions that motivate large #s of folks years to a lifetime off planetMusk is a marketeer; looking cool is important to selling the dream & human satisfaction......
Quote from: philw1776 on 11/28/2016 07:36 pmMy guesses at SpaceX site criteria0. Low enough below mean datum for sufficient aerobraking for landing (-2Km or lower) & low enough latitude (under ~30 degrees) to minimize landing & takeoff delta V. Excess landing deltaV makes colony $/ton landed freight bill more expensive. More trips/thousand tons. Excess takeoff deltaV consumes more energy intensive ISRU resources.1. ISRU: water available in colony need quantities2. ISRU: solar power available in colony quantities as mining water and especially disassociation eats electrons3. Given 1&2 sufficient water & solar power available for colony4. Other ISRU needs: minerals etc. for colonial development5. Interesting site & nearby attractions that motivate large #s of folks years to a lifetime off planetMusk is a marketeer; looking cool is important to selling the dream & human satisfaction......I am becoming sold on the idea that low elevation for landings is a higher priority than water. Water ice can be transported but elevation is hard to change.
Mind you that recently there is evidence that the "rocky" is likely ... surface ice! Which would be ideal for ISRU, as a bulldozer might effectively collect enough water for ISRU. And ... there may be enough of a crustal magnetic field. which along with the increased atmospheric density ... would have the least radiation (and perchlorate) issues for habitation.But here are the problems - likely static effects and dust accumulation is largest too, so optical density/scattering would be the worst on Mars. Also, solar would have the lowest yield due to the inclination.
......The inclination should not have too much effect with canted solar arrays, though with initial arrays only rolled out on the ground. Canted solar arrays should help reduce dust accumulation.I have also thought later, though not early, solar arrays could be located in the highlands, much reducing dust problems.
Quote from: MickQ on 11/27/2016 10:28 amUtopia Planitia may be boring BUT it has a basically unlimited water supply. IMO, the ideal place to set up the solar and ISRU plants needed. Plenty of area to build an initial base to establish a foothold. Plenty of room to locate landing zones far enough away from other structures. So what if you have to drive 10klm from the ITS to the base. It's not hard with the right vehicles.Land, get set up safe and comfortable and then worry about science and exploration.Do you want to live in New England (hills, valleys, waterfalls, lakes, forests, etc.) or in Kansas/Nebraska?
Do you want to live in New England (hills, valleys, waterfalls, lakes, forests, etc.) or in Kansas/Nebraska?
Quote from: DOCinCT on 12/03/2016 07:28 pmQuote from: MickQ on 11/27/2016 10:28 amUtopia Planitia may be boring BUT it has a basically unlimited water supply. IMO, the ideal place to set up the solar and ISRU plants needed. Plenty of area to build an initial base to establish a foothold. Plenty of room to locate landing zones far enough away from other structures. So what if you have to drive 10klm from the ITS to the base. It's not hard with the right vehicles.Land, get set up safe and comfortable and then worry about science and exploration.Do you want to live in New England (hills, valleys, waterfalls, lakes, forests, etc.) or in Kansas/Nebraska?Do you want to live, full stop?
Wanted to draw attention to this:A possibly interesting site for large payload landing is Hadriacus Palus, which is just east of Terby crater on the very northern edge of Hellas Planitia.
Paul Wooster, SpaceX, on Mars landing site selection: looking at sites at latitudes < 40˚, elevation as low as possible. #LPSC2017
Wooster: identified several candidate sites, but many likely too rocky. Arcadia region looks promising. #LPSC2017
Wanted to draw attention to this:A possibly interesting site for large payload landing is Hadriacus Palus, which is just east of Terby crater on the very northern edge of Hellas Planitia. It has a latitude of 27.25 South which is within the 30S cutoff for solar power considerations - it also has probable water ice deposits, nearby mineral deposits, and generally high scientific value - leading to it being ranked 16th out of all the landing sites in the 2020 workshop:Evaluation paper here:http://www.hou.usra.edu/meetings/explorationzone2015/pdf/1052.pdf
Amazonis Planitia. < 40˚ latitude, low elevation, not too rocky, and highest water ice concentrations at that latitude.
But if there's lots of water in other forms, then focus should be on power.
Here's Jeff Foust's write-up of Paul's Woosters comments:http://spacenews.com/spacex-studying-landing-sites-for-mars-missions/
Quote from: Dao Angkan on 03/20/2017 02:45 amAmazonis Planitia. < 40˚ latitude, low elevation, not too rocky, and highest water ice concentrations at that latitude.That's pretty sweet to learn. If the priority is ice not a bad choice. It looks like a mix of both Amazonis and Arcadia technically; then again most of the northern plains may as well just be counted as one giant extension of Vastis Boreallis. As I stated in the Red Dragon thread, other regions could just as easily suffice if this is just an engineering test but I have to admit if the priority is ice (and eventually setting up a colony) the region is a very fair choice.That map you posted also show a surprising number of southerly sites. What is known about them?
Not good for solar power in winter. Not exactly exciting topography for settlers. The "fun" factor Elon oft mentions.Perhaps SpaceX wants earliest RD missions to have easiest ice access to validate ISRU tech and then proceed to base selection forays.Also NASA landing site priority criteria are not likely SpaceX's priorities.
Isn't it "easy" to tip the solar panels making higher latitude almost as good. I would think dust on the panels or in the air might be a more important power consideration.
Quote from: philw1776 on 03/20/2017 04:44 pmNot good for solar power in winter. Not exactly exciting topography for settlers. The "fun" factor Elon oft mentions.Perhaps SpaceX wants earliest RD missions to have easiest ice access to validate ISRU tech and then proceed to base selection forays.Also NASA landing site priority criteria are not likely SpaceX's priorities.First of all we don't know the conop for the mission. It might not be intended to survive the winter. Or it might be powered down over winter. Or the panels might be tilted to allow winter operations. We don't even know whether Red Dragon will run on solar power. It might rely on batteries and have a surface mission that lasted only a few days.
More on the Space News web site. Gives details of some other landing sites considered - Deuteronilus Mensae, Phlegra Montes and Utopia Planitia - all ruled out because they were too rocky. Interesting that Utopia, where Viking 2 landed, was considered to be unsuitable. Indicates the surface roughness tolerance on the landing system to below Viking 2 levels.See more at: http://spacenews.com/spacex-studying-landing-sites-for-mars-missions/
Quote from: rsdavis9 on 03/20/2017 01:50 pmIsn't it "easy" to tip the solar panels making higher latitude almost as good. I would think dust on the panels or in the air might be a more important power consideration.You can fix the elevation angle, but can't fix the shorter days.I'm with RB here. If we're stuck with solar, maximizing power is the #1 consideration. With water, all you need is to pass a certain threshold, not maximize - and I think you can pass that threshold in many locations.
Quote from: meekGee on 03/21/2017 02:43 pmQuote from: rsdavis9 on 03/20/2017 01:50 pmIsn't it "easy" to tip the solar panels making higher latitude almost as good. I would think dust on the panels or in the air might be a more important power consideration.You can fix the elevation angle, but can't fix the shorter days.I'm with RB here. If we're stuck with solar, maximizing power is the #1 consideration. With water, all you need is to pass a certain threshold, not maximize - and I think you can pass that threshold in many locations.Remember the following:1) We don''t the power requirements, or how it might be supplied.2) Shorter daylight in winter is balanced by longer daylight in summer. Power usage can be adjusted accordingly. Viking 2 data (similar latitude) indicates that surface irradiance varies between 0.3 and 4 kwh/m2. Assuming 30% efficiency that is 0.1-1.3 kwh/day
Quote from: Dalhousie on 03/22/2017 10:16 pmQuote from: meekGee on 03/21/2017 02:43 pmQuote from: rsdavis9 on 03/20/2017 01:50 pmIsn't it "easy" to tip the solar panels making higher latitude almost as good. I would think dust on the panels or in the air might be a more important power consideration.You can fix the elevation angle, but can't fix the shorter days.I'm with RB here. If we're stuck with solar, maximizing power is the #1 consideration. With water, all you need is to pass a certain threshold, not maximize - and I think you can pass that threshold in many locations.Remember the following:1) We don''t the power requirements, or how it might be supplied.2) Shorter daylight in winter is balanced by longer daylight in summer. Power usage can be adjusted accordingly. Viking 2 data (similar latitude) indicates that surface irradiance varies between 0.3 and 4 kwh/m2. Assuming 30% efficiency that is 0.1-1.3 kwh/dayPersonally, I'm hoping they'll go with nuclear, but that's a separate issue.The total energy requirement are reasonably well known. Tons of methane per BFS, liters of O2 per person, etc.
Quote from: meekGee on 03/22/2017 10:41 pmQuote from: Dalhousie on 03/22/2017 10:16 pmQuote from: meekGee on 03/21/2017 02:43 pmQuote from: rsdavis9 on 03/20/2017 01:50 pmIsn't it "easy" to tip the solar panels making higher latitude almost as good. I would think dust on the panels or in the air might be a more important power consideration.You can fix the elevation angle, but can't fix the shorter days.I'm with RB here. If we're stuck with solar, maximizing power is the #1 consideration. With water, all you need is to pass a certain threshold, not maximize - and I think you can pass that threshold in many locations.Remember the following:1) We don''t the power requirements, or how it might be supplied.2) Shorter daylight in winter is balanced by longer daylight in summer. Power usage can be adjusted accordingly. Viking 2 data (similar latitude) indicates that surface irradiance varies between 0.3 and 4 kwh/m2. Assuming 30% efficiency that is 0.1-1.3 kwh/dayPersonally, I'm hoping they'll go with nuclear, but that's a separate issue.The total energy requirement are reasonably well known. Tons of methane per BFS, liters of O2 per person, etc.I don't there is any chance of anything nuclear (except perhaps RHUs) flying to Mars on the 2020 Red Dragon.
The thread comments can be confusing. Some of us are referring to colony site landing sites while others are referring to RD landing sites. The criteria could be quite different, e.g. lack of solar irradiance circa 40 degrees north might not be a big issue for a RD mission, but could be a big negative for an all-seasons colony, assuming no nukes.
Quote from: philw1776 on 03/23/2017 03:21 pmThe thread comments can be confusing. Some of us are referring to colony site landing sites while others are referring to RD landing sites. The criteria could be quite different, e.g. lack of solar irradiance circa 40 degrees north might not be a big issue for a RD mission, but could be a big negative for an all-seasons colony, assuming no nukes.IMO it is a safe assumption that a RedDragon landing site would be chosen to be a likely colony site.Maybe not for a 2018 like mission where landing was the main/only goal. But for 2020 missions. If the choice was right, then a first ITS can use a radio beacon from that landing to home in on.
Nor do I! It makes sense, I guess, to put a Red Dragon with a beacon at the colony site before we start pre-landing the habitat and supplies, but allowing for a wee bit of a delay that would likely be a decade from now (minimum), so all the early dragons will be doing other things. They are already being promoted as delivery of customer cargo, so the sites will be chosen to suit the customers for quite a while.
I just argue from the timeline given. I am aware that the timeline will slip, like everybody is. But presently they are working towards it. That does not leave any room. 2020 for Red Dragon. 2022 for the unmanned ITS. That timeline means the 2020 Red Dragons are direct precursors for the first colony flights. Remember there is the need to build substantial capacity for fuel production at that first landing site. They don't do that randomly for any number of locations until they like one for settlements.That does not mean they would not abandon the first site if it for some reason turns out to be untenable but it would be a major and costly setback.I don't just assume Elon Musk is only talking nonsense about his plans.
Quote from: guckyfan on 03/24/2017 06:47 amI just argue from the timeline given. I am aware that the timeline will slip, like everybody is. But presently they are working towards it. That does not leave any room. 2020 for Red Dragon. 2022 for the unmanned ITS. That timeline means the 2020 Red Dragons are direct precursors for the first colony flights. Remember there is the need to build substantial capacity for fuel production at that first landing site. They don't do that randomly for any number of locations until they like one for settlements.That does not mean they would not abandon the first site if it for some reason turns out to be untenable but it would be a major and costly setback.I don't just assume Elon Musk is only talking nonsense about his plans.When it comes to timelines, he talks nothing but nonsense. There is also a huge difference between a Red Dragon mission which could feasibly launch in 2020 (although may well slip to 2022 based on record) and the ITS fantasies.So let's stick to Red Dragon landing sites.
Quote from: Dalhousie on 03/24/2017 09:58 amQuote from: guckyfan on 03/24/2017 06:47 amI just argue from the timeline given. I am aware that the timeline will slip, like everybody is. But presently they are working towards it. That does not leave any room. 2020 for Red Dragon. 2022 for the unmanned ITS. That timeline means the 2020 Red Dragons are direct precursors for the first colony flights. Remember there is the need to build substantial capacity for fuel production at that first landing site. They don't do that randomly for any number of locations until they like one for settlements.That does not mean they would not abandon the first site if it for some reason turns out to be untenable but it would be a major and costly setback.I don't just assume Elon Musk is only talking nonsense about his plans.When it comes to timelines, he talks nothing but nonsense. There is also a huge difference between a Red Dragon mission which could feasibly launch in 2020 (although may well slip to 2022 based on record) and the ITS fantasies.So let's stick to Red Dragon landing sites.Red Dragon is hardly less of a fantasy. SpaceX will pursue ITS until it goes bankrupt, at which point Red Dragon missions will stop, too.Not long ago, folks would say VTVL and Red Dragon were fantasies. And ITS is the reason for these Red Dragon missions anyway.
I think you are mistaken on several counts. When proposed jointly by NASA and SpaceX Red Dragon was clearly feasible with technology either proven or under development and within the framework of current budgets.
The justification of Red Dragon is not ITS with which it has almost nothing in common. Red Dragon is a way of commercially transporting payloads to Mars.There are plenty of ITS threads. Let's focus on Red Dragon here.
Quote from: Dalhousie on 03/25/2017 05:40 amI think you are mistaken on several counts. When proposed jointly by NASA and SpaceX Red Dragon was clearly feasible with technology either proven or under development and within the framework of current budgets. Yes and it involved a number of proposed NASA missions using Red Dragon capabilities, none of which were followed up on so far.Quote from: Dalhousie on 03/25/2017 05:40 amThe justification of Red Dragon is not ITS with which it has almost nothing in common. Red Dragon is a way of commercially transporting payloads to Mars.There are plenty of ITS threads. Let's focus on Red Dragon here.This is where you go wrong IMO to an extent that is completely incomprehensible to me. The Red Dragon missions as proposed by SpaceX are an integral part of their Mars plans. Precursors to ITS missions. Just look at the slides of the IAC announcement by SpaceX. They are part of the Mars timeline.That does not rule out the possibility that NASA could purchase Red Dragon flights for their own missions in the future. Even once ITS has landed, that covers just one location. There are no doubt many locations that could still be explored by robot missions.
I understand the skepticism that SpaceX will succeed. I do NOT understand the skepticism that SpaceX is actually serious about their stated intentions. They may be crazy, but they're sincere.Red Dragon is about ITS and settling Mars. Full stop.
...It plain enough. Red Dragon has been marketed specifically as a commercial systems for flying paying payloads to Mars.ITS could never happen, could be a complete failure, or could be delayed for a decade or more with little impact on the Red Dragon program.
Quote from: Dalhousie on 03/25/2017 07:53 am...It plain enough. Red Dragon has been marketed specifically as a commercial systems for flying paying payloads to Mars.ITS could never happen, could be a complete failure, or could be delayed for a decade or more with little impact on the Red Dragon program.You omitted the possibility that ITS could be a success. Red Dragon is a precursor flight or flights for the follow-on ITS program -- Dragon has minimal utility in its present configuration other than the vehicles will already be paid for by crew and cargo flights. It will fly until a dedicated design Mars spaceship replaces it.
Quote from: AncientU on 03/25/2017 11:37 pmQuote from: Dalhousie on 03/25/2017 07:53 am...It plain enough. Red Dragon has been marketed specifically as a commercial systems for flying paying payloads to Mars.ITS could never happen, could be a complete failure, or could be delayed for a decade or more with little impact on the Red Dragon program.You omitted the possibility that ITS could be a success. Red Dragon is a precursor flight or flights for the follow-on ITS program -- Dragon has minimal utility in its present configuration other than the vehicles will already be paid for by crew and cargo flights. It will fly until a dedicated design Mars spaceship replaces it.I think the point is, as far as currently known, SpaceX is specifically seeking a site for landing a Red Dragon. That's it....for now.Unless Elon Musk speaks loudly and specifically, we can only presume the Arcadia/Amazonis Planitia site is for the first Red Dragon. The 2nd and onward Dragons could fly to the top of Olympus Mons, or ITS to the bottom of Hellas Planitia likewise as far as we know. Inversely the site could be useful for a colony...but there's no confirmation, only interest for the first Red Dragon landing site. The only other given is that the Red Dragon technically could land most places on Mars if the vendor is willing. We can guess, not much else.End of line.
Wooster, who is involved in Mars mission planning in addition to his “day job” as manager of guidance, navigation and control systems on SpaceX’s Dragon spacecraft, said that site selection is based on several criteria. One is access to large quantities of ice near the surface that could, ultimately, support human settlements.Another is to be close to the Equator and at a low elevation for solar power and better thermal conditions. “It’s probably hard to find that along with ice,” he acknowledged, so the focus has been on four locations at latitudes no more than about 40 degrees from the Equator.
Those landing sites are of particular interest, he said, for SpaceX’s long-term vision of establishing a human settlement on Mars, but he said the company wouldn’t rule our sending Red Dragon spacecraft elsewhere on the planet to serve other customers. “We’re quite open to making use of this platform to take various payloads to other locations as well,” he said. “We’re really looking to turn this into a steady cadence, where we’re sending Dragons to Mars on basically every opportunity.”
Red Dragon's stated purpose (besides building SpaceX's Mars EDL tech--for ITS) is to test ISRU technology, specifically some kind of water extraction. They need this ISRU for ITS, no other reason.
There are no "commercial" payloads to Mars except SpaceX's own ISRU payloads to prepare for ITS. That's 95% of the purpose of Red Dragon.
Quote from: redliox on 03/25/2017 11:58 pmQuote from: AncientU on 03/25/2017 11:37 pmQuote from: Dalhousie on 03/25/2017 07:53 am...It plain enough. Red Dragon has been marketed specifically as a commercial systems for flying paying payloads to Mars.ITS could never happen, could be a complete failure, or could be delayed for a decade or more with little impact on the Red Dragon program.You omitted the possibility that ITS could be a success. Red Dragon is a precursor flight or flights for the follow-on ITS program -- Dragon has minimal utility in its present configuration other than the vehicles will already be paid for by crew and cargo flights. It will fly until a dedicated design Mars spaceship replaces it.I think the point is, as far as currently known, SpaceX is specifically seeking a site for landing a Red Dragon. That's it....for now.Unless Elon Musk speaks loudly and specifically, we can only presume the Arcadia/Amazonis Planitia site is for the first Red Dragon. The 2nd and onward Dragons could fly to the top of Olympus Mons, or ITS to the bottom of Hellas Planitia likewise as far as we know. Inversely the site could be useful for a colony...but there's no confirmation, only interest for the first Red Dragon landing site. The only other given is that the Red Dragon technically could land most places on Mars if the vendor is willing. We can guess, not much else.End of line.Selection criteria are specifically for settlement per SpaceX. Please don't ignore the only data point we have been provided.
QuoteWooster, who is involved in Mars mission planning in addition to his “day job” as manager of guidance, navigation and control systems on SpaceX’s Dragon spacecraft, said that site selection is based on several criteria. One is access to large quantities of ice near the surface that could, ultimately, support human settlements.Another is to be close to the Equator and at a low elevation for solar power and better thermal conditions. “It’s probably hard to find that along with ice,” he acknowledged, so the focus has been on four locations at latitudes no more than about 40 degrees from the Equator.There is interest in sending Red Dragons to other sites for paying customers, but that isn't why this site selection is being done.
QuoteThose landing sites are of particular interest, he said, for SpaceX’s long-term vision of establishing a human settlement on Mars, but he said the company wouldn’t rule our sending Red Dragon spacecraft elsewhere on the planet to serve other customers. “We’re quite open to making use of this platform to take various payloads to other locations as well,” he said. “We’re really looking to turn this into a steady cadence, where we’re sending Dragons to Mars on basically every opportunity.” http://spacenews.com/spacex-studying-landing-sites-for-mars-missions/
Quote from: Robotbeat on 03/26/2017 04:37 amRed Dragon's stated purpose (besides building SpaceX's Mars EDL tech--for ITS) is to test ISRU technology, specifically some kind of water extraction. They need this ISRU for ITS, no other reason.However the experiment is realsitically be supplied by NASA who have the experitise here. Which means that its has broader application than SpaceX fantasies.
Quote from: Robotbeat on 03/25/2017 03:31 pmI understand the skepticism that SpaceX will succeed. I do NOT understand the skepticism that SpaceX is actually serious about their stated intentions. They may be crazy, but they're sincere.Red Dragon is about ITS and settling Mars. Full stop.So are Mars one.
This mission will primarily be an engineering test to see if they can actually land. Anything extra will be a bonus. Incidentally, Arcadia is marginally closer to the poles than the equator.
Quote from: Dalhousie on 03/26/2017 11:11 pmQuote from: Robotbeat on 03/25/2017 03:31 pmI understand the skepticism that SpaceX will succeed. I do NOT understand the skepticism that SpaceX is actually serious about their stated intentions. They may be crazy, but they're sincere.Red Dragon is about ITS and settling Mars. Full stop.So are Mars one. Correct. Mars One is serious (I think) about their ambitions. Doesn't mean they'll succeed.
So, how far is reasonable to travel from the launch site? I'm presuming that the best site for landing is unlikely to be the best site for a colony. If landing in Amazonis at a latitude of 35° N where would you head towards? It looks flat enough that you might be able to head south all the way to the equator, or maybe head south east towards Olympus Mons. I think it's roughly 300km every 5°, so how far should we expect vehicles to be able to travel? Maybe you'd have to set up battery charging stations every xxxkms.
Imagine if we had a thread about Mars One landing site but didn't actually want to talk about sites Mars One wanted to land.
Long term solar arrays at high altitude and spaced 7000km east and west would solve both dust storm and night storage problems. There would always be one of 3 sites in full sun.
Thick deposits cover broad regions of the Martian mid-latitudes with a smooth mantle; erosion in these regions creates scarps that expose the internal structure of the mantle. We investigated eight of these locations and found that they expose deposits of water ice that can be >100 meters thick, extending downward from depths as shallow as 1 to 2 meters below the surface. The scarps are actively retreating because of sublimation of the exposed water ice. The ice deposits likely originated as snowfall during Mars’ high-obliquity periods and have now compacted into massive, fractured, and layered ice. We expect the vertical structure of Martian ice-rich deposits to preserve a record of ice deposition and past climate.
Let's send some robo-drill rigs and settle this once and for all...
Problem is that this ice is still at high latitudes ~55 degrees. Bad for solar especially in LONG winter. Need nukes.
this is a big deal because there’s a considerable amount of this mantling material on Mars at about 30 degrees latitude in both hemispheres
So in addition to finding the shallowest water ice deposits known on Mars, the researchers are also the first to observe active erosion of the Martian midlatitude ice scarps.
Quote from: philw1776 on 01/11/2018 10:03 pmProblem is that this ice is still at high latitudes ~55 degrees. Bad for solar especially in LONG winter. Need nukes.From the gizmodo.com articleQuotethis is a big deal because there’s a considerable amount of this mantling material on Mars at about 30 degrees latitude in both hemispheres QuoteSo in addition to finding the shallowest water ice deposits known on Mars, the researchers are also the first to observe active erosion of the Martian midlatitude ice scarps.
Quote from: philw1776 on 01/11/2018 10:03 pmProblem is that this ice is still at high latitudes ~55 degrees. Bad for solar especially in LONG winter. Need nukes.I was wondering.. is it really that bad if you find a nice mountainside facing the equator? Even at Louth crater ( ~70°) where white ice is visible from orbit, I think you are at least avoiding the long uninterupted night of a polar winter, and one rim of the crater would be nicely angled towards the sun.It would be good to know what the drop of efficiency of solar panels around 55° is. I think this could be mainly dictated by the time the sun is beneath the horizon. You do not have to lie it flat on the ground. So long as the sun is above the horizon you can angle your panels to directly face it. This can reduce dust gathering as well. You have lots of free space so you could lay them out in one very long wall instead of a more sensible square; so that they will not occlude the panels behind them.
You said it in your post. The problem at high latitudes is that for the LONG Martian winter the sun is below the horizon fo the vast majority of hours per day. Angling panels does not help with this. The game is Kilowatt HOURS.
It’s got thicker atmosphere, probable glaciers, and isn’t too bad latitude wise. Probably on the short list.
So anyone think Elon is going to staked out Hellas soon?
You can't feed one million people from hydroponics. They are going to want eggs and meat from poultry, milk, beef and dairy products from cattle, pork, bread, vegetables, beer, whiskey and wine. This means several hundred thousand chickens, a 100,000 cows, a 100,000 swine, and about 2 million acres in cultivation as practiced on Earth. High intensity ag might reduce the total land by a factor of, say, 4 to 500,000 acres.
History tells us that poorly resourced colonies fail. We have to think big for a one million person civilization on Mars, and at some point nuclear (or fusion) power will be needed to make it all happen.
I'm reasonably sure that the best Martian colonists can hope for, is lab grown meat and fish from a combined aquaponic system. Anything else would be a huge waste of resources, that the colony won't be able to afford for a very long time.
There is one problem that no one mentioned. A large amount of water ice close to the surface of the ground can mean that when heated this ice will melt, and the ground will turn into liquid mud. This is called "permafrost". Permafrost is well known to northern peoples. In such a ground, it is very difficult to build underground structures.
This is - somewhat - less relevant than on earth.
Quote from: Valerij on 02/12/2018 10:12 amThere is one problem that no one mentioned. A large amount of water ice close to the surface of the ground can mean that when heated this ice will melt, and the ground will turn into liquid mud. This is called "permafrost". Permafrost is well known to northern peoples. In such a ground, it is very difficult to build underground structures.This is - somewhat - less relevant than on earth.On earth, you can get away with less insulated structures that warm the ground noticably.On Mars, unless you have a fusion plant, underground structures need to be very, very well insulated, as the average subsurface temperature at the equator is about -50C, and 20C colder at middle-latitudes, to under -100C at the polar caps.
The atmosphere of Mars is the layer of gases surrounding Mars. It is composed mostly of carbon dioxide. The atmospheric pressure on the Martian surface averages 600 pascals (0.087 psi; 6.0 mbar), about 0.6% of Earth's mean sea level pressure of 101.3 kilopascals (14.69 psi; 1.013 bar). It ranges from a low of 30 pascals (0.0044 psi; 0.30 mbar) on Olympus Mons's peak to over 1,155 pascals (0.1675 psi; 11.55 mbar) in the depths of Hellas Planitia. This pressure is well below the Armstrong limit for the unprotected human body
Quote from: speedevil on 02/12/2018 10:23 amQuote from: Valerij on 02/12/2018 10:12 amThere is one problem that no one mentioned. A large amount of water ice close to the surface of the ground can mean that when heated this ice will melt, and the ground will turn into liquid mud. This is called "permafrost". Permafrost is well known to northern peoples. In such a ground, it is very difficult to build underground structures.This is - somewhat - less relevant than on earth.On earth, you can get away with less insulated structures that warm the ground noticably.On Mars, unless you have a fusion plant, underground structures need to be very, very well insulated, as the average subsurface temperature at the equator is about -50C, and 20C colder at middle-latitudes, to under -100C at the polar caps.Liquid water can not exist on mars unless inside a pressurized space or container,,, Heating water ice will only see it vanish to vapor as it passes roughly 0*C (32*F)...There is No Mud on Mars... I assure you... QuoteThe atmosphere of Mars is the layer of gases surrounding Mars. It is composed mostly of carbon dioxide. The atmospheric pressure on the Martian surface averages 600 pascals (0.087 psi; 6.0 mbar), about 0.6% of Earth's mean sea level pressure of 101.3 kilopascals (14.69 psi; 1.013 bar). It ranges from a low of 30 pascals (0.0044 psi; 0.30 mbar) on Olympus Mons's peak to over 1,155 pascals (0.1675 psi; 11.55 mbar) in the depths of Hellas Planitia. This pressure is well below the Armstrong limit for the unprotected human bodySource...https://en.wikipedia.org/wiki/Atmosphere_of_MarsOn Edit...Heating martian permafrost will cause it to dry out... because of the low atmospheric pressure...
Quote from: John Alan on 02/12/2018 10:43 amQuote from: speedevil on 02/12/2018 10:23 amQuote from: Valerij on 02/12/2018 10:12 amThere is one problem that no one mentioned. A large amount of water ice close to the surface of the ground can mean that when heated this ice will melt, and the ground will turn into liquid mud. This is called "permafrost". Permafrost is well known to northern peoples. In such a ground, it is very difficult to build underground structures.This is - somewhat - less relevant than on earth.On earth, you can get away with less insulated structures that warm the ground noticably.On Mars, unless you have a fusion plant, underground structures need to be very, very well insulated, as the average subsurface temperature at the equator is about -50C, and 20C colder at middle-latitudes, to under -100C at the polar caps.Liquid water can not exist on mars unless inside a pressurized space or container,,, Heating water ice will only see it vanish to vapor as it passes roughly 0*C (32*F)...There is No Mud on Mars... I assure you... QuoteThe atmosphere of Mars is the layer of gases surrounding Mars. It is composed mostly of carbon dioxide. The atmospheric pressure on the Martian surface averages 600 pascals (0.087 psi; 6.0 mbar), about 0.6% of Earth's mean sea level pressure of 101.3 kilopascals (14.69 psi; 1.013 bar). It ranges from a low of 30 pascals (0.0044 psi; 0.30 mbar) on Olympus Mons's peak to over 1,155 pascals (0.1675 psi; 11.55 mbar) in the depths of Hellas Planitia. This pressure is well below the Armstrong limit for the unprotected human bodySource...https://en.wikipedia.org/wiki/Atmosphere_of_MarsOn Edit...Heating martian permafrost will cause it to dry out... because of the low atmospheric pressure... This may be true on the surface but underground the water has no where to sublime to.
Quote from: Restless on 02/09/2018 04:57 amYou can't feed one million people from hydroponics. They are going to want eggs and meat from poultry, milk, beef and dairy products from cattle, pork, bread, vegetables, beer, whiskey and wine. This means several hundred thousand chickens, a 100,000 cows, a 100,000 swine, and about 2 million acres in cultivation as practiced on Earth. High intensity ag might reduce the total land by a factor of, say, 4 to 500,000 acres.I'm reasonably sure that the best Martian colonists can hope for, is lab grown meat and fish from a combined aquaponic system. Anything else would be a huge waste of resources, that the colony won't be able to afford for a very long time.
Liquid water can not exist on mars unless inside a pressurized space or container,,, Heating water ice will only see it vanish to vapor as it passes roughly 0*C (32*F)...There is No Mud on Mars... I assure you... ...On Edit...Heating martian permafrost will cause it to dry out... because of the low atmospheric pressure...
Agree that a water rich but otherwise loosely (sediment) structured substrate won't turn to mud, but as the water sublimes, it may become considerably weaker. So some thought needs to be given to where to build and how deep to excavate, etc.
If melt water penetrates ...