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Well the Curiosity's top speed is 0.14 Km per hour. So, I was being cautious. If you've got some precious cargo you're towing, I think you'd probably want to go pretty slowly. Once the boulders and rocks are cleared, then yes much faster speeds should be possible.
Louis,
I can't think of any reason why rovers can't travel at a slow walker's pace on flat and level ground. If 5kph is as fast as a rover can manage, then you're better off bunny hopping along in .38g. I think 20kph is a more reasonable travel speed for a human operated rover. If the ground really is that littered with debris, such that it would impede a rover traveling at parking lot speeds, then you're not landing BFS there.
Anything that requires the level of effort associated with the construction of the solar power array is not a sacrificial tool. The BFS integrated propellant plant may not see service as a rocket afterwards, but it performs a vital function for crew return and serves as a source of spare engine parts for the passenger carrying BFS.
Last edited by louis (2018-06-30 16:33:06)
Let's Go to Mars...Google on: Fast Track to Mars blogspot.com
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One disruptive technology we've talked about since year 2000: quantum entanglement communicator. Using electrons contained in a quantum well on a microchip. It's been tested with photons in a fiber-optic cable, it works. Theoretically photons should have infinite range, electrons will have a finite range, but no one know how to calculate that. Advantage of electrons is no cable. This is similar technology as quantum computing, but not exactly the same. It would provide instantaneous communication over whatever distance it works. Real time communication to a rover means a human operator on Earth can drive it. That allows a lot faster drive. It also allows telepresence. So why hasn't it been done? And don't tell me it can't work because tests with fiber-optic cable already worked, and quantum computing is progressing.
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Robert,
I'm sure anything can be done with enough time, money, and research effort, but counter-factual quantum communication using the Quantum Zeno effect was only experimentally achieved last year. There's at least another decade of effort before a reliable communications system is ready for testing.
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The InSight lander is currently generating about 0.5 KwHs per sq. metre per sol in a non-optimal insolation zone.
On that basis a PV array of 100 metres by 100 metres, 10,000 square metres, would generate 5,000 KweH or 5 MweHs. I would estimate that with that you could generate steady power throughout the day (using batteries, or methane/oxygen generation) of say 0.25 Mwe or 250 KweHs for a human mission to Mars. However with a PV powered mission you would design it so that power was used mostly at PV peak, rather than lose lots of power to battery generation. So, you'll probably see power being used at 1Mw during the peak period - that would be when you heat water, run the dishwasher, produce propellant, recharge rover batteries etc. You'd probably see power used in the range of maybe 125 Kwes to 1,000 Kwes."
To produce 1000 tons of propellant you need an averaged constant of around 122 Kwes throughout the sol for 700 sols (although of course that's the average - the power intake could vary to some degree). So a 10,000 square metre PV field could meet that requirement, but you would need possibly to increase it slightly to allow for the impact of any prolonged dust storms. The real constraint is not so much the power output but rather how big you make your propellant manufacturing kit - I am presuming the more you make it fit peak power output, the more mass of equipment you require. So although you might have 1.25 Mwes to spare, you might not want 10 times the size of kit suitable for steady power output at 125 Kwes. So you need battery or other storage to ensure constant output and a PV system you do have to factor in dust storm outage which could reduce insolation for 80% at the extreme, certainly by 40% over months in worst case scenarios.
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Louis,
Some years ago now, a local robotics competition for high school students included a challenge to sweep dust off solar panels. I have noticed the absence of robots on Mars to perform that function. That's not a criticism of course, because the missions currently on Mars have been scrubbed of non-essential functionality. However, the next generation might well include robots dedicated to maintenance of solar panel arrays. A potentially useful cleaning method would be jets of atmosphere across the panels, to try to reduce abrasion of the surface of the panels.
Edit: If a private enterprise were looking for a project, to test a solar panel cleaning robot, here is a suggestion:
https://mars.nasa.gov/mer/mission/statu … tyAll.html
(th)
The InSight lander is currently generating about 0.5 KwHs per sq. metre per sol in a non-optimal insolation zone.
To produce 1000 tons of propellant you need an averaged constant of around 122 Kwes throughout the sol for 700 sols (although of course that's the average - the power intake could vary to some degree). So a 10,000 square metre PV field could meet that requirement, but you would need possibly to increase it slightly to allow for the impact of any prolonged dust storms.
Last edited by tahanson43206 (2018-12-09 07:53:17)
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I think that has been an assumption of previous discussions - that there will be a system to remove dust from the panels. Of course rovers haven't had the benefit of service robots. I think they have relied on some gradient manouevres to remove the dust. If we have ultralightweight PV film suspended on angled wires, tugging at the wire would probably be enough to shake off a lot of dust.
Louis,
Some years ago now, a local robotics competition for high school students included a challenge to sweep dust off solar panels. I have noticed the absence of robots on Mars to perform that function. That's not a criticism of course, because the missions currently on Mars have been scrubbed of non-essential functionality. However, the next generation might well include robots dedicated to maintenance of solar panel arrays. A potentially useful cleaning method would be jets of atmosphere across the panels, to try to reduce abrasion of the surface of the panels.
Edit: If a private enterprise were looking for a project, to test a solar panel cleaning robot, here is a suggestion:
https://mars.nasa.gov/mer/mission/statu … tyAll.html(th)
louis wrote:The InSight lander is currently generating about 0.5 KwHs per sq. metre per sol in a non-optimal insolation zone.
To produce 1000 tons of propellant you need an averaged constant of around 122 Kwes throughout the sol for 700 sols (although of course that's the average - the power intake could vary to some degree). So a 10,000 square metre PV field could meet that requirement, but you would need possibly to increase it slightly to allow for the impact of any prolonged dust storms.
Let's Go to Mars...Google on: Fast Track to Mars blogspot.com
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So mission to resurect opportunity and Spirit, such a repair mission could not only be a proof of concept but to stop the calls of hoax from those that do not believe.
For Mars Loui solar Watt Hours are not guaranteed and we should not count of it being the case...
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I believe it's true all the solar powered rovers have extended their lifetimes way beyond the original designated target - sometimes by 10x or more.
So mission to resurect opportunity and Spirit, such a repair mission could not only be a proof of concept but to stop the calls of hoax from those that do not believe.
For Mars Loui solar Watt Hours are not guaranteed and we should not count of it being the case...
Let's Go to Mars...Google on: Fast Track to Mars blogspot.com
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Survival of solar powerd robots will and are not the same as for human life.
Here is the solar power comparison for what we have sent...
Pheonix had the same panels but due being so far north and winter it could not survive....
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Up until recent we have had large solid panels, the atk fan and a flexible plastic substrate cell format but the work of nasa is pushing for a roll our array as well. I believe that the cell plate is not flexible but the fabric that its attached to is.
https://www.nasa.gov/offices/oct/home/feature_sas.html
https://www.nasa.gov/mission_pages/stat … /2139.html
The space test was done at the ISS using the canadian arm...
https://www.pv-magazine.com/2017/06/23/ … -in-space/
https://www.space.com/37250-roll-out-so … ation.html
The system uses a rail to extend the length of the array and a means to push it outward plus the roller that the array is wrapped on.
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June of 2017 and silence about the test it would seem...
https://en.wikipedia.org/wiki/Roll_Out_Solar_Array
https://ntrs.nasa.gov/archive/nasa/casi … 005379.pdf
https://www2.jpl.nasa.gov/adv_tech/phot … ES1976.pdf
https://ntrs.nasa.gov/search.jsp?R=20130008777
The Flexible Array Concentrator Technology (FACT) is a lightweight, high-performance reflective concentrator blanket assembly that can be used on flexible solar array blankets
https://sbir.gsfc.nasa.gov/printpdf/31223
Materials and Structures Optimization / Process ... - NASA
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Great news...looks like perfect timing for the Space X Mars Mission.
Would be interesting to see some figures for Earth orbit generation - Whs per sq metres per hour and per kg at peak in Earth orbit, so we can extrapolate to Mars.
June of 2017 and silence about the test it would seem...
https://en.wikipedia.org/wiki/Roll_Out_Solar_Array
https://ntrs.nasa.gov/archive/nasa/casi … 005379.pdf
https://www2.jpl.nasa.gov/adv_tech/phot … ES1976.pdf
https://ntrs.nasa.gov/search.jsp?R=20130008777
The Flexible Array Concentrator Technology (FACT) is a lightweight, high-performance reflective concentrator blanket assembly that can be used on flexible solar array blankets
https://sbir.gsfc.nasa.gov/printpdf/31223
Materials and Structures Optimization / Process ... - NASA
Let's Go to Mars...Google on: Fast Track to Mars blogspot.com
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Found why we did not hear much about this experiment...
Farewell, ROSA! Space Station Lets Go of Roll-Out Solar Array After Retraction Fail (Video)
After a week of tests on the end of the International Space Station's robotic arm, the Roll-Out Solar Array (ROSA) was safely jettisoned. While the rollable solar panel unfurled successfully at the beginning of the experiment, the ground operations team was unable to retract it to stow.
https://spaceflightnow.com/2017/06/30/p … trip-home/
ROSA was extracted with the station’s Canadian-built robotic arm and extended to a length of more than 15 feet (4.5 meters).
The solar array unfurled June 18, extending like a party favor with tensioning booms on both sides of the 5.5-foot-wide (1.6-meter-wide) wing.
Developed by Deployable Space Systems of Goleta, California, in partnership with the Air Force and NASA, the Roll-Out Solar Array tested solar cells capable of generating up to 300 watts of electricity. But future versions of the solar panel could extend to much greater lengths, producing as much as 500 kilowatts of power, according to Banik.
ROSA solves this problem by reducing mass by 20 percent and reducing stowed volume by 400 percent over these traditional approaches.”
1.6 x 4.5 = 7.2 m^2 for an output of 300w is horrible.... its 1300 w for each meter of input just 3% of what it could be doing....that has got to be a heat caused issue for how low the power output is....
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I think that Spaceflightnow article must have got garbled somewhere along the line. No way can that figure be right. It's probably the individual panel sections are generating 300ws peak. Or maybe it was 3000ws? 30% would be about right.
I've searched here there and everywhere but can't find any figures on power generation but I think it is safe to assume it's going to be around 30% of insolation.
I think on Mars we could save on structure by either deployed directly on the ground (weighing down with rocks) or by rolling out PV film on lightweight wire structures stretched between poles.
Found why we did not hear much about this experiment...
Farewell, ROSA! Space Station Lets Go of Roll-Out Solar Array After Retraction Fail (Video)After a week of tests on the end of the International Space Station's robotic arm, the Roll-Out Solar Array (ROSA) was safely jettisoned. While the rollable solar panel unfurled successfully at the beginning of the experiment, the ground operations team was unable to retract it to stow.
https://spaceflightnow.com/2017/06/30/p … trip-home/
ROSA was extracted with the station’s Canadian-built robotic arm and extended to a length of more than 15 feet (4.5 meters).
The solar array unfurled June 18, extending like a party favor with tensioning booms on both sides of the 5.5-foot-wide (1.6-meter-wide) wing.
Developed by Deployable Space Systems of Goleta, California, in partnership with the Air Force and NASA, the Roll-Out Solar Array tested solar cells capable of generating up to 300 watts of electricity. But future versions of the solar panel could extend to much greater lengths, producing as much as 500 kilowatts of power, according to Banik.
ROSA solves this problem by reducing mass by 20 percent and reducing stowed volume by 400 percent over these traditional approaches.”
1.6 x 4.5 = 7.2 m^2 for an output of 300w is horrible.... its 1300 w for each meter of input just 3% of what it could be doing....that has got to be a heat caused issue for how low the power output is....
Let's Go to Mars...Google on: Fast Track to Mars blogspot.com
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We have talked about the laying on the ground drops the amount that the array will produce as it needs to be perpendicular to the suns rays. Also now it will be dusted all the time and further reducing the level of out put between cleanings.
https://www.civicsolar.com/support/inst … rgy-output
The effect of an array's tilt angle on solar PV energy output may be up to 20% compared to that of flat installations. A comparison of data in two US cities has been completed to exhibit the importance of a solar PV arrray's tilt angle.
https://www.solarchoice.net.au/blog/fla … -vs-tilted
Small variations away from these ideals will not result in a significant difference in the power output of your solar energy system, which is why the natural tilt angle of your roof is usually fine (and keeping that tilt frames can add significantly to the cost of your system, putting a damper on the value of the solar power it produces).
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I don't think you mean "perpendicular" Spacenut...looks like 30 degree tilt is optimal. You could get that from a hillside. But of course that would then require your landing location to have convenient south facing hillsides within perhaps 1 km and laying out would be a bit of a struggle. If you went with laying out, I think you would choose flat ground. Yes there is a loss, but in terms of mass carried to Mars then there is a plus side, given you minimise structure.
But I think my preferred method would be laying ultralightweight PV on wires strung between poles (rather like you get in a vinyard). That way you can get your 30 degree tilt. The structure can be very lightweight as the weather on Mars presents no real problems - apart from the extreme temperature but that is a given for space-rated PV I would presume. Also, with PV film on wires, you can probably clear most dust simply by "twanging" the wires (vibration has proved very effective in getting rid of unwanted dust on robot missions, I understand). A robot rover could simply go up and down the line all sol long operating some twanging mechanism.
We have talked about the laying on the ground drops the amount that the array will produce as it needs to be perpendicular to the suns rays. Also now it will be dusted all the time and further reducing the level of out put between cleanings.
https://www.civicsolar.com/support/inst … rgy-output
The effect of an array's tilt angle on solar PV energy output may be up to 20% compared to that of flat installations. A comparison of data in two US cities has been completed to exhibit the importance of a solar PV arrray's tilt angle.
https://www.solarchoice.net.au/blog/fla … -vs-tilted
Small variations away from these ideals will not result in a significant difference in the power output of your solar energy system, which is why the natural tilt angle of your roof is usually fine (and keeping that tilt frames can add significantly to the cost of your system, putting a damper on the value of the solar power it produces).
Let's Go to Mars...Google on: Fast Track to Mars blogspot.com
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Ya perpendicular to the suns incoming rays....
u is the position of the sun relative to the face of the panel t
the angle is chosen from the definition of plum which intersects the right angle at the panel sun alignment point
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Apologies SpaceNut! My misreading.
Ya perpendicular to the suns incoming rays....
http://tse1.mm.bing.net/th?id=OIP._6pAy … d=3.1&rm=2u is the position of the sun relative to the face of the panel t
the angle is chosen from the definition of plum which intersects the right angle at the panel sun alignment point
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I can get things wrong.....and no worries as this is a good topic to know what we have researched and learned together as a group.
I do hope the ROSA cells did perform better than the article indicate efficiency as they would save mass for mars. Also like you indicated a few poles set in the ground with guide wire to support it would be as good as we can get for aligning them at the location required angle. Also by being flexible the angle can be altered as the season changes to keep the output as high as it can be even in winter....
With the aid of reflective materials to redirect the sun we can even think about boosting the output or the array as well.
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Bumping for technology developement of which if its going to be solar only then this should be an important document if it have been linked here.
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A while ago I went and brought 2 solar powered sensed lighting units. One has the standard solar cells in clear with LED light, with the other having a solar cell that is difused plastic with cob leds. The difused plastic versus the glass is inferior to amount of light from a charge but for the experiment testing we are looking at predictable light from chaging when both are in the same environment.
I have been placing them outside in the sunlight with the alignment to the sun and on days that is overcast raining horizontal or level. The time for a full day for each have been monitored over weeks for each trial with the results being somewhat disappointing for the light duration from a day of charge.
While the rainy difused light is longer the intensity of the light to charge results in less than an evening duration and is most of the time about 2 hours of light from either at the most. This is the effect of a mars dust filled sky where the light intensity is difused. But on days that are clear the time when level does improve by at least an hour more of duration of light. But its the aligning of the cells toward the sun giving the most time of duration again with an additional 2 or more hours over the level condition.
The clear unit results with the difused unit not doing so well
difused level days charge = 2hrs total run time of light output for charge
light not cloudy level = 3hrs
light aligned = 6hrs or more
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For Louis re topic ...
Here is (or appears to be) good news about advances in fabrication of multi-spectrum solar cells.
https://www.yahoo.com/finance/news/did- … 00117.html
(th)
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The materials are different in each layer which collect some of the energy from each range of color frequencies of the light passing through it. These are multi junction which we are using on mars rovers and landers. I have seen articles indicating that 8 layers would collect more energy but the added mass is what makes them not worth doing..
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Articles on solar and storage here
https://www.motherearthnews.com/renewable-energy
The reason solar farms on Earth have to be so robust is the weather on Earth: hurricanes, tornadoes, rain storms, hail storms etc etc The weather on Mars is benign with the wind force being something like 1/20th that on Earth, so even a 60 MPH wind (top recorded I think) has puny effects.
My favoured solution is to have wires suspended between poles (probably just two parallel wires will suffice) and then hang the very lightweight PV film (off a roll) on to the wires (probably using hooks). How you secure the poles will need some attention.
kbd512 wrote:Louis,
Maybe we could have robots that are capable enough to setup the materials in the rough locations required and then humans could arrive and make all the electrical connections or final adjustments using hand tools. If that's what you meant by automation, then yeah, I could see that happening. That said, we're going to have to plan on EVA's. If the plan is to just sit back and watch robots work, then we can do that from the comfort of Earth where no lives are at risk.
Given how long it takes to set up a solar farm on Earth with unlimited manpower and equipment, we're going to need a well-rehearsed plan, lots of practice with setup of real solar arrays wearing real pressurized space suits, and maybe some kind of helper robots or machines that follow the crew around feeding rolls of PV or wiring to them so they can simply make electrical connections as fast as they can.
louis posts 11 12 replies
Mars branding of items made there is a means but we can do that now with nothing being brought from mars at all as fakes sell just as good as the real stuff would.
A rock is a Rock either here or mars as its only gravity that will be different for moving it as they are the same materials. Mining on mars will be more dangerous as we have no air to breath, that fragments could puncture the space suit, and that automated equipment will be slower and breakdown requiring more eva's to repair increasing risk.
Tension wires (steel cable) break when the mass is blown by wind and that will break the panels wires as well. That said louis calculate the size wire (steel cable) that you will bring for mass for tension and wiring of the panels from earth its total lengths to support all of the panels plus all of the poles needed to anchor it in place.
Rollout thin film plastic panels (12% - 15% eff.) are less efficient and require twice if even more panels than fixed glass (25% - 35% eff.) which will survive the mars weather where as the plastic type will not.
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