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See above GW - the Lab Padre film in the Spacexcentric video shows that a number of the landing legs didn't deploy, didn't lock into position. Could that be the result of the fire maybe distorting the mechanism?
As best I understand it, when Spacex shuts down a Raptor, they stop one propellant flow first, and thus quench the chamber fire by its lack, with the other propellant still running. I don't know which one is first, but I'd guess methane first, then oxygen. Then they shut it off, too. The engine expels the cooler gas to fully depressurize, just at lowered velocity. These expelled gases mix with the air in the engine bay for a short time. Not zero, but short.
If my guess about how Raptors shut down is correct, the engine bay is enriched in oxygen for that time. Any fuel leakage would be very flammable and extremely easy to ignite. Or any solid material in the bay that was smoldering for any other reason, would brighten up and burn faster for a time.
I would not think they would shut off the oxygen first, because that would fill the bay immediately with methane fuel. That guarantees a huge fire as air percolates back in. Any source of ignition, even just hot parts, can set off the conflagration. Methane is almost as notorious as hydrogen about easy ignition. (It's also almost as notorious as hydrogen about being easy-to-leak.)
What I saw with SN-10 was "good" until they completed the flip back to vertical. When they shut down two of the engines, there was a very large fire visible, streaming out of the bay, continuously all the way to the ground, as it descended on the one engine. That means there was a rather significant leakage flow of methane into the bay, feeding the large fire. I think this fire was big enough to do significant damage to plumbing and wiring. It would also heat up the thin sheet metal that is the "thrust puck", but which is also the main oxygen tank.
When it got near the pad, there was too much dust and smoke for me to see anything until the cloud cleared after the landing. Then it was quite clear the ship was standing roughly 5 degrees out of plumb. Which in turn means there was something wrong with some, but not all, the landing legs. All those on one side were "short" in some way.
I find that landing leg trouble unsurprising, to say the least. I don't know how they are operated, but either plumbing or electricity (or both) are used. Doesn't matter which, it was exposed to a big fire in the bay for a significant time, and fire is hell on wiring or plumbing. Odds are the bay fire caused the leg malfunction.
I did see it standing there with a small fire showing on the higher side of the base of the tilted ship. It burned like that for a while, until sometime after they shot a water stream into the vicinity of the ship. If there was still a fire burning in the bay, that was not visible from outside. I think there was still an ongoing fire in the bay, that it was leaking methane burning with air in the bay, and that it finished burning a hole in the thrust puck/oxygen tank.
When the oxygen hit the methane-air fire in the bay, ka-boom! Which is why the bay walls and aft fins were ripped from the ship, with the explosion pressure wave lifting the entire ship around a hundred meters skyward. That was a fast deflagration by the way, not-at-all a detonation! Those are even more powerful. By far. There would be no recognizable ship left, just small pieces, if that had been a detonation.
They really, really need to get control of leaking methane and the raging engine bay fires it can so easily cause. That's three prototypes fundamentally destroyed by this issue. Could be faulty valves, leaking pipe joints, or even welds cracking. It has long been known (over a century now) that many of those things which perform perfectly well in ground tests, often come apart under real-world stresses in flight. Usually stresses not accounted-for in the design analysis. Usually also causing loss of the craft.
Boeing and P&W are currently suffering from exactly that, with the P&W4000 hollow fan blade cracking problem. And not just on those B-777's that use that engine. It's on some other airplanes, too.
As for the landing leg design, well, I have offered my assessment about that before (and it was not, and still is not, at all good). The first time one of these vehicles makes a forced landing off-site, without that flat reinforced concrete pad, well, the resulting loss of vehicle (and maybe crew) will induce them to do that job better. The longer they put that off, the more expensive it will become.
You won't get to choose what you land upon, in an emergency. It might be a soft sand dune or a bog of soft mud. Or a plowed field. Or a golf course with water hazards. You had best design for this ahead of time. Why? Because nothing is as expensive as a dead crew, especially one dead from a stupid management decision.
GW
I think you are underestimating the extent to which NASA can (a) identify hard level rock surfaces (to a depth of many metres) and (b) identify rocks on the surface using computerised analysis of repeat photos (different orbits) of the same area. IIRC correctly they can resolve down to about 60cms.
Remember as well that Space X are sending cargo ships first so when they land they can make v. detailed images of the landing area, selecting the best for the human landers. With automated rovers on board, they can even clear away rocks.
Anyway, all this can be tested on Earth first, and the Moon later. I think a lunar landing will be more difficult than a Mars landing.
The illustrates the need for a concrete pad as well since rocks that are in the field of landing can not be predicted to not damage the engines and with the surface not level it makes the problem even greater. This problem is not just for mars but for a version that is for the moon as well since there is the regolith sink depth that will need to be accounted for....
SpaceXcentric's latest video - includes a segment from Lab Padre showing the failed deployment of all legs - a few didn't lock. Might also explain why they couldn't quench the fire as the Starship body was in contact with the ground - no space to get at the engines.
Mars a dark world? Try living under the tree canopy on Earth that still covers much of the planet! Hardly any cloud cover on Mars either.
As on Earth the energy budget is not necessarily the decisive cost - labour often is. If you've got to ship hundreds of people to the Moon and then look after them in order to set up say a methane-oxygen plant, you might well find it still makes sense to send the stuff from Earth.
For me, the Moon is clearly destined to be a major tourist destination but I think at the same time there will be a strong "lunar preservation" movement on Earth (especially as the Moon still has religious significance for hundreds of millions of people), so I think any tourist facilities will need to be "discreet" (probably covered in lunar dust in some way). I see no particular reason why the Moon should become an industrial centre, given the proximity of the Earth and competition from Mars. I think Mars, for instance will be a better location for methane manufacture for rockets, to be transferred to LEO and LMO.
The Moon has power from solar etc to make it a major space factory for us. But food growth sorry a 28 day cycle seriously screws this.
Mars though a dark world has an atmosphere of CO2 that can be used to grow plants and with a low gravity can supply the whole solar system with less cost than any launch from earth.
Ceres is in the asteroid belt with almost no gravity but we can carve into it and we can utilise those meteor belt objects to provide very rich materials to anywhere we can make it and that also includes the Moon and Mars orbit.
It is called triangle trade but it really is not. It is orbital dynamics that moving materials using the least amount of energy wins every time. Powered cargoes will be by tugs using the most efficient engines and currently we are talking a variant of long use electric-Ion engines
Thanks for the clarification - makes sense!
Louis,
The use of plain water has nothing whatsoever to do with "looking cool". You may be obsessed with "looking cool", but engineers probably aren't. AFFF (Aqueous Film-Forming Foam) is used on liquid petroleum fires, such as kerosene fires. As someone who's actually sprayed AFFF on an actual DFM (Diesel Fuel Marine) fire, I have a pretty good appreciation for what it can and can't do. It wouldn't do anything at all to prevent a gas like Methane from escaping from beneath the AFFF, which is intended to act as a vapor seal between vaporized and liquid kerosene or fuel oil distillates.
Edit:
AFFF is also pretty useless for fighting gasoline-fueled fires, which is why it doesn't get used on those, either. If the rocket in question was loaded with RP-1, then SpaceX should have some kind of AFFF system installed in the landing area. Since they're actually using Methane, having AFFF is pointless. The water can cool hot metal components and interrupt combustion from direct contact, but the surface film that AFFF creates over fuel oils can't prevent volatile gases like Methane from vaporizing and continuing to combust. The rule of thumb is AFFF for kerosene, diesel, or bunker fuel. AFFF would also work on a coal / wood / plastic fueled fire, but water is every bit as effective there, so again, there's no point to doing that.
One question:
Why don't space facilities smother the rocket with fire suppressant foam as used in airliner crashes by fire services? Wouldn't that be more effective? One suspects that it might be because it won't look "cool". "Cool" is a major design concern in rocketry.
I agree about the legs...stability is going to be a big issue going forward, so why not address the landing legs issue now?
Unfortunately, the ability to post-flight examine the Raptor engines went up in a ball of flames. I guess there was still significant amount of Methane left in the fuel tanks?
The issue with the rinkydink landing legs needs to be addressed pretty soon. I'm in favor of Falcon-style folding legs with a much wider "footprint," as well as more ground clearance.
I agree with GW about having some fiberglass insulation and foil to protect the vulnerable engine plumbing. Maybe they don't care if they lose a prototype, but this last incident shows there's still a way to go with the Raptor engines reliability.
JUst catching up with things...it subsquently exploded/imploded after a pretty good if slightly bumpy landing.
I was misled by the Space X commentator into thinking they had abandoned the launch attempt for the rest of today but no - they tried again and succeeded!
Amazing achievement. 10 Km flight and faultless landing.
Obviously I'm not a rocket scientist but I think they've accomplished already the three most difficult parts of an orbital flight - the launch, the flip and the landing.
So I guess the booster is the next critical stage...?
Anyway, Space X have once again shown themselves to be true pioneers. Orbital flight this year looks very possible if bureaucratic interference can be avoided.
2021 Non human Starship to orbit
2022 Human Starship to orbit
2022-2023 Lunar circumnavigation and possible lunar surface landing with humans together with Starship test landings on Mars analogue rock slabs or on rock fields on Earth.
2023 - 2025 Testing of all Mars human mission systems e.g. hab unloading and erection, use of Rovers, life support systems, drilling for water ice, methane production, coms etc etc.
2024 - Mars cargo landings
2026 Humans to Mars
I was misled by the Space X commentator into thinking they had abandoned the launch attempt for the rest of today but no - they tried again and succeeded!
Amazing achievement. 10 Km flight and faultless landing.
Obviously I'm not a rocket scientist but I think they've accomplished already the three most difficult parts of an orbital flight - the launch, the flip and the landing.
So I guess the booster is the next critical stage...?
Anyway, Space X have once again shown themselves to be true pioneers. Orbital flight this year looks very possible if bureaucratic interference can be avoided.
2021 Non human Starship to orbit
2022 Human Starship to orbit
2022-2023 Lunar circumnavigation and possible lunar surface landing with humans together with Starship test landings on Mars analogue rock slabs or on rock fields on Earth.
2023 - 2025 Testing of all Mars human mission systems e.g. hab unloading and erection, use of Rovers, life support systems, drilling for water ice, methane production, coms etc etc.
2024 - Mars cargo landings
2026 Humans to Mars
At 0 seconds! First time I've ever seen that. A testament to modern computing power I guess!
Abort!
Felix (WAI site) has a Live Stream on the SN10 launch which will happen soon we hope.
Latest helpful update from Felix (WAI):
I was always quite taken by the atom bomb rocket. You just have a succession of atom bombs that are periodically placed on the "engine" side of a big radiation shield. Each one accelerates the craft. I guess you could fine tune so G forces aren't too bad. Can't recall the name given to the concept. It's not Nerva. I seem to recall the atom bomb rocket could get you up to interstellar speed pretty quickly.
As an hard SF writer, I was looking for a realistic starship for my next novel which will be set between the local stars. The ship should be about 600 ton of mass and she should be able to reach Proxima in about 16-17 years, traveling at 0.25 C.
Can we build such a ship with slightly ameliorated current technologies?
After making some rough math, I found the answer and I was quite shocked: yes we can build it using a laser sail like the mini probe of Yuri Milner, but bigger.
A 600 ton starship needs almost 880 TW of optical laser power to accelerate at 1 g.
We can image a one-micron-thick carbon-carbon sail, coated with 10 nm of molibdenum on the aft side: such a sail would weight 0.0018 kg/m2 and would have a power load of 100 MW/m2 at 2000 K. So the total sail area would be 8814000 m2, the diameter 3350 m (or a square of 2970 m of side) and the mass 15.9 ton. The sail would be furled like the sail of JAXA's IKAROS: stowed on a rolling drum like an origami, then extended and kept in shape by centrifugal force. We can image carbon nanotubes artificial muscles, embedded in the sail as stiffening ribs, that fold it again during the coasting phase of the trip.
The ship will have also four fission reactors for electrical power, a 20 T superconductive magnetic coil to shield the habitat from GCR, a passive shielding of 30 cm of water, ten one-micron-thick carbon-carbon shields for space dust, laser as point defense against debris, lidars radars and quite powerful chemical RCS rockets to dodge bigger objects.
The accelerating laser array will be build on the polar regions of Mercury: the best diode lasers have a plug to wall efficiency of 76% and we can imagine they might reach 90%. So to have 880 TW of optical power we need 978 TW of electrical power, that become 1632 TW due to the red shift, to keep the ship accelerating at the same rate when she reaches relativistic speeds (at 0.25 C a 216 nm laser becomes 360 nm so the beam power is at 60%).
With a constant acceleration of 1 G and 0.25 C of cruise speed, the acceleration phase ends 5765 AU away from the Sun, so the laser array needs an aperture of almost 120 km (imagine a field of lasers of 120 km of diameter) to be focused on a sail of 3350 (the lasers have 216 nm of wavelength).The photovoltaic array will be put near the equator: at Mercury the sun power is 6600 W/m2. We can image that in a near future solar panels will become 85% efficient: so to get 1632 TW of electrical power we need a square array of panels of 1386 km of side, and we need many of these due to the rotation of the planet.
Laser and solar PP also need radiators.
All this stuff will be very expensive and difficult to build, but not impossible.
The weak point of my dream is that my spaceship needs also a laser deceleration station in the orbit of the destination star.
We can imagine three possibilities: they are built in our solar system then sent to the destination system at 0.03 C with a fission-fragment propelled spaceship. They are built in the destination system with local materials after sending robots. They are built in the destination system by intelligent aliens in communication with us.
It seems like over-egging the pudding to talk about propellant production. Why would you take CO2 from Mars if you can make your propellant on the ground in Mars?
If it can be built (and I really don't see why it can't...it would be a lot simpler than the ISS). I don't really see why you couldn't assemble it automatically, given a car can park itself. Transponders could get the units into close proximity, then lasers could fine tune the couplings and strong magnets could bring the units together in perfect alignment. In-place bolt systems could then be activated once you have the units properly aligned.
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Voyager Station(s), a little more.
Others may have already gathered the information I will put here.
One thing is they will not recycle water back to humans. Instead they plan to make propellants out of it. That sort of makes some sense, as they can sell the propellants, and their high end customers will not have to think about drinking other peoples recycled fluids.
Even though it is highly probable that every time we drink water it is water that passed through other creatures bodies in the past. Still a pretty smart move, I think. So for raw materials, for propellants they would have available cast off water fluids, and CO2 exhaled by humans. So how much Hydrolox, how much Metholox do they create?
I presume that at first they lift up the food that is to be fed to the clients. Later, then maybe farm "Worlds" near by? I wonder what the Carbon cycle will be like? No need for Carbon phobic weirdos on this please. Don't know if Carbon from Mars would be competitive or not. Maybe if it were a farm product, the farms in orbit, the CO2 from that atmosphere.
And eventually, the water from the Moon? Not at first though.
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Also, for radiation protection they plan to make some kind of an ice shield. And they may be considering magnetic protections as well, not sure on that.
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These "Pilot Programs" are to be precursors to such devices being deployed all over the solar system, according to them. I guess I believe that solar would be possible at Jupiter with concentrating mirrors, and maybe even Saturn/Titan/ect.
But eventually I guess some kind of nuclear would need to figure in.
As I see it, a companion farm type device, could be built from inner system rocky materials, and then pushed out twards large ice deposits, and filled with water.\
In the case of smaller moons for Saturn, Uranus, and Neptune, eventually some of those moons would be strip mined all the way down to rocky materials by this method.
From there, I guess a method for Pluto/ect.
Or the robots kill us all
I will probably be dead anyway at that point. Almost certainly.
But until dead, dreams can be nice.
Done.
https://www.dailymail.co.uk/sciencetech … -2025.html
Any views on how realistic this proposal is?
I am so much more excited about the Starship programme than the Perseverance Rover!
Hmmm...re the New Atlas story, Emrod seem to making a lot of inflated claims when theircurrent prototype transmits "Just a few watts. Our current prototype is relatively small. It transmits about 40 meters (130 ft). "
The Japanese invested a lot more in this technology and I think got to the position of transmitting over maybe 1 or 2 Kms but development seems to have stalled.
To go from having a 40 metre prototype to claiming there are no major obstacles to transmitting from a geosyncrhonous solar power satellite stationed 36,000 kms away seems a bit bizarre to me.
I hope the development programme goes well but I don't think we are anywhere near beamed solar power from satellites yet.
Here is a set of links provided by a relative, when I asked what he thought about Solar Power Satellites.
The response I received was surprisingly positive. It included concern about possible risks, but leaned toward concern about saving the environment from fossil fuel use.
I haven't followed these links yet, but trust that they are on point.
https://www.allaboutcircuits.com/news/w … rom-space/
https://www.electronicdesign.com/power- … less-power
https://ijeir.org/administrator/compone … _Final.pdf
https://newatlas.com/energy/wireless-po … interview/
(th)
I may be wrong but I think the examples you are quoting relate to radar and radio and are not really relevant because the initial power source becomes diffuse. The most powerful radio transmitter in the world is in any case only 2MW - similar to the capacity of a single, not largish wind turbine.
Meaningful in this case stands for "suggesting that this could be a practical source of energy in the short to middle term". No one disputes you can transfer energy by laser or microwave - it's just a question of how much, how effeciently and at what cost. If we can overcome the technical challenges it will be brilliant.
For Louis re #16 --- thanks for confirming you've been following the field ...
I noted your use of the word "meaningful" .... that is a reasonable choice, as I think about it, because (of course) humans have been sending "meaningful" RF for over 100 years.
December 12, 1901
On December 12, 1901, Marconi attempted to send the first radio signals across the Atlantic Ocean, in spite of predictions that the radio waves would be lost as the earth curved over that long distance.A Science Odyssey: People and Discoveries: Marconi ... - PBS
www.pbs.org › wgbh › aso › databank › entriesI understand you meant something other than "meaningful" so I'll give you the benefit of the doubt.
The energy required to send a signal to Voyager had to have been on the order of what is required for a power delivery application.
Military radar systems that can observe objects in LEO and beyond are also operating at power levels comparable to those required for this application.
These systems have been operating for many decades ...
June 17, 1935
It is historically correct that, on June 17, 1935, radio-based detection and ranging was first demonstrated in Britain. Watson Watt, Wilkins, and Bowen are generally credited with initiating what would later be called radar in this nation.History of radar - Wikipedia
(th)
Re EVs you're ignoring that once you have an electric road infrastructure with induction charging of vehicles on the move, EVs win out on range and convenience. You can also then have a much lower battery weight onboard which means the vehicle itself will be much cheaper. The idea it will remain a rich guy's toy is absurd.
We shall see over the next five years whether you are correct regarding a 2026 manned landing.
Tesla stocks are trading at P/E of 1300. That means 1 cent of earnings for every $13 of shares. It is one of the highest PE ratios in history. If Tesla were producing something unique and revolutionary and were destined to become the biggest car maker in the world, that might be sustainable. But there are plenty of other competitors. And as things stand, electric cars are a rich man's toy. They are not easily affordable to most people and it is doubtful that they ever will be in their present form. Their market share is therefore small. If we face another big recession and a substantial reduction in employment and average earnings, Tesla could easily go bankrupt.
Introducing the EV is going to be an uphill struggle, because the laws of physics are against you. The difference between electric cars and previous innovations, is that this is a technology that is undeniably inferior in its performance compared to what it is trying to replace. It's high cost and range issues both have their roots in the same basic problem: the poor energy density of electrochemical batteries. This isn't a problem for which there is an easy solution. And it is being introduced at a time when tge average person is growing progressively poorer, due to the deteriorating energy dynamic of the economy. Tesla have done their best to work around the inherent problems of battery electric, by using Li-ion batteries and developing a frame and chassis that is light and low drag. The result is a very mediocre vehicle that is twice as expensive as competing IC driven car. Governments can virtue signal all that they want. But banning IC engines will not make the EV more affordable to ordinary people.
The above discussion applies to cars and light vehicles. The difficulties involved in introducing electric power into goods transport are even more daunting.
Re food:
How you grow your food will depend on the population numbers. Early on there will be no problem using indoor agriculture with artificial lgihting. When pressurised greenhouses become necessary we can move into that sort of farming. They don't have to be earth pressure - they can be near 100% CO2 and about 20% of earth atmospheric pressure - allowing transparent plastics to be used. We can use lightweight reflectors to increase insolation into the farm domes. You can also build in farms into hillsides, again reducing construction costs.
I really don't see the need to be base the diet on algae.
The Mars Republic will have a whole planet to dip into! It won't really be that easy to intimidate into compliance from Earth.
Musk's plan clearly relies on shipping out huge amounts of industrial equipment to kickstart the local economy. Mars will be the most invested-in economy anywhere in the solar system - the per capita amounts of investment will be off the scale...US per capita capital investment was something like $60,000 per capita in 2017. In the early Mars community you will be talking more about $6 million per person in a community of 5,000, a hundred times more...at least! These sorts of levels of capital equipment, reflected in things like robot mining equipement, life support tech, 3D printers, service robots etc. will provide a strong platform for further growth. I think Mars will be surprisingly independent of Earth imports at a very early stage. There will be a strong financial incentive to make it so, given the costs of importation.
Choice of food will ultimately be driven by consumer preference. But there are a number of reasons why I would expect microalgae to dominate the food supply in early Martian settlement phase. Firstly, there is simple economics. Land based vegetable plants must be grown in pressurised greenhouses. The total area needed per person is quite large and they (may) need to be heated at night. This makes vegetable plants relatively expensive on Mars and cereal crops very expensive. Microalgae in contrast, can be grown in 3d printed plastic panels on the surface. You would need about a third of the total area compared to a greenhouse growing vegetables and you can drain the panels into an insulated tank overnight. So no absolute need for heating, though it may boost productivity. There are thousands of different edible microalgae. Not all of them are unpleasant to taste. As most human food is now processed, it will make little difference to the consumer whether the pasta on their plate comes from an algae panel or a field of wheat. But the price they pay will be very different. In a competitive market, the cheapest solution usually wins. Finally, microalgae are more nutritious than most land crops, because nutrition is not diluted by superfluous structure. So I think that by the 23rd century, this will be a normal food source and land plants and meat will be seen as niche.
I don't know when the optimum time will be for Mars to declare independence. But I doubt it will be taken kindly by the Earth government elites. These people tend to be hostile towards regimes that they cannot directly control. The US reaction towards Russia expelling Jewish oligarchs being a good example. Even with all of the natural resources and land that Russia has, the US restrictions imposed on it has an impact on the prosperity of its people. If you are stuck on an airless planet, where all botanical products and many technology products must be imported, a trade embargo could be devastating. Of course, that might not be an issue if the Mars government policies just happened to be approved of by Earth political elites. If it was a woke establishment, controlled by Earth approved oligarchs, for example. But I accept the fact that that is unlikely to be appealing to most people. The question is, how far along does a Mars colony have to get, before it can do without the approval of these people? If Mars is providing something essential, that cannot easily be substituted from other sources, it could be soon. If it is instead one nation amongst many, it may take a while.
I don't think Mars will need to control population numbers for a long time to come. If population pressures increase, then space based manufacturing will provide abundant new living space by the 23rd century. In fact Mars may struggle to maintain a large resident population, when the asteroid belt offers so many more opportunities. The Belta Lowda may turn out to be the most prosperous people in the solar system.
Nope. No chance. I've followed this before in the last 5 years or so - because I would love this to be a practical technology - and I checked out the latest on Google and Wikipedia. Nothing much has changed. Meaningful wireless transmission of energy has only been demonstrated over something like a kilometre IIRC.
For Louis ... re Post #11
By any chance, are you (possibly?) a few decades behind in your references?
We are talking about distances on the order of 1000 miles (1600 km) or less, as compared to the GEO distance of 22,236 miles (35,786 km).
I'll be very interested in any trustworthy reporting on actual experiments with RF transmission over 1000 miles or less.
Humans have a ** lot ** of experience transmitting (and receiving) RF over that distance.
(th)
Sadly this technology doesn't yet appear practical for reasons of energy loss in conversion and cost. Some progress has been made but it's very slow.
Following up on #8 ...
There is no reason why a particular location on Earth could not be supplied with abundant SPS power from LEO.
In post #7, the existence of a class of polar orbits that are always in sunlight was considered for delivery of power to a location on Earth for 30 minutes every 24 hours.
There is no reason that I can see for why there could not be multiple satellites in this particular polar orbit.
Each satellite would be busy sending power to fixed locations along its track, so the satellite would never be without a destination for collected energy.
The cost of delivery of power to the ground stations would thus be divided among the ground stations.
If a given satellite has an orbital period of 90 minutes ( and I do ** not ** know what the orbital period of a sun synchronous satellite might be) then there would be three stations along the track to receive power. With 48 satellites in operation, there would be 3 x 48 or 150 - 6 or 144 ground stations in the network. As a reminder (for myself, in particular) the Sun Synchronous orbit plane passes through the center of the Earth. Satellites in that orbit can serve locations on Earth that are experiencing sunset (on one side of the Earth) and sunrise (on the other).
Many of these receiving stations would be on islands, where power could be collected and used to make useful products like hydrogen and oxygen, or whatever the market might find valuable.
A few locations might be on floating platforms where that would make economic sense.
The same principle could apply to Mars, with the distinct difference there are no oceans to worry about.
Edit #1 - SPS in LEO could be spaced every degree of latitude, or perhaps even more closely. Each could serve three clients for 30 minutes on a given orbit.
Service could be modified by demand through control from ground stations managing the network.
If there are 360 satellites (which seems reasonable (at least to me)) then they would serve 360 * 3 or 900 + 180 or 1080 ground stations in each orbit.
But the Earth is rotating underneath, so the total number of ground stations to be served would be greater.
I'm not sure how many ground stations could be served, but I'm assuming that at a minimum, 24*60 minutes divided by 90 minutes (16) tracks are possible.
That would yield 1080 * 16 service opportunities in 24 hours for 360 satellites. pr 17,280 in all.
Edit#2: Google came up with this citation from Wikipedia for Sun Synchronous Polar Orbits ...
Typical Sun-synchronous orbits around Earth are about 600–800 km in altitude, with periods in the 96–100-minute range, and inclinations of around 98°. This is slightly retrograde compared to the direction of Earth's rotation: 0° represents an equatorial orbit, and 90° represents a polar orbit.
Sun-synchronous orbit - Wikipedia
en.wikipedia.org › wiki › Sun-synchronous_orbitEdit#3: Google came up with this estimate of the diameter of the Earth pole-to-pole
Image result for diameter of earth pole to pole
Equatorial vs Polar Diameter:
Because of this, the diameter of the Earth at the equator is about 43 kilometers (27 mi) larger than the pole-to-pole diameter. As a result, the latest measurements indicate that the Earth has an equatorial diameter of 12,756 km (7926 mi), and a polar diameter of 12713.6 km (7899.86 mi).Jun 14, 2008What is the Diameter of Earth? - Universe Todaywww.universetoday.com › diameter-of-earth
Circumference would be 24906 miles, so locating satellites every 100 miles would allow only 249.
Separating the satellites every 10 miles would allow for more interesting total of 2490.
That number times 16 yields 39840 power delivery opportunities.
Thus, the cost of 2490 satellites would be distributed over 39840 ground stations, each of which would receive 30 minutes of delivered solar power each day.
The cost of the ground stations would include storage capability, to allow the 30 minutes of input to be metered out over 24 hours.
Flow batteries might be a good fit for this application.
(th)
Given virtually every major government has committed to electric road transport by 2040 I can't see Tesla shares going anywhere but north. But, yes, the unexpected can happen. But even in the Great Depression of the 1930s, new industries like electricity generation and automobile manufacture continued to grow.
I think you are being way too pessimistic. There is no doubt Musk wants this done at Apollo project speed. Space X and he have the money.
The rate at which they are knocking out Starships and their rockets is phenomenal. Improvements are being made all the time.
If they achieve orbital by end 2021, then I really can't see major obstacles, assuming (a) no legal or administrative barriers are put in place and (b) NASA co-operate with him on communications, satellite imagery and all other necessary facilities.
If NASA refused to co-operate that could delay things as he would have to get other countries to help him and/or build his own facilities. But so far everything suggests NASA/JPL have been co-operating very closely with Space X e.g. on potential landing sites.
A human landing by 2026 seems eminently doable. It would mean mastering some basic ISRU, solar energy generation on the surface, methane and oxygen production on Mars, EVAs, maintenance and return launch of a Starship, hab facility assembly, and life support technology. Sounds daunting but most of the technology is already in place.
All else being equal, another decade could see men walk the sands of Mars. However, I doubt that all else will be equal. What if the world gets hit by another great recession or even a great depression and Tesla becomes junk stock? Musk would have to scale back his space ambitions dramatically, as much of his paper wealth would disappear very quickly. In fact, I think this is the most likely scenario. First footsteps on Mars could be mid century, or maybe never at all.
Why have a population of 6.7 billion eating processed pulp when you could have a population of 1 billion eating the most delicious range of fresh foods? What you need is a population policy, not one based on enforcement but on incentives either towards large families or smaller families, depending on where you are. I think a population of 1 billion is more than enough to sustain an Earth-like world economy.
Mars with about 40% of Earth's insolation could easily support a population of billions. And of course if we are talking about 2300 then by that point I am sure we will have mastered how to reflect huge amounts of solar radiation on to the planet, so bringing it up to Earth levels, if we so wish.
I am an Early Independencer, believing that the Mars community founded by Space X should declare itself independent at the earliest opportunity. Even if there are only 5000 people there, they should make the declaration of independence. It should be a self-governing democracy. Any future settlements should be subject to its approval and to those settlements joining the Republic on the the terms laid out in the constitution.
The alternative is to see Mars become a playground for dictatorships, oligarchs and religious fanatics.
According to your video, there is a fairly consistent answer, which is 100 -150 years after first settlement. So that would put independence towards the end of the 22nd century, or beginning of 23rd.
They envisage the transition of power being gradual and peaceful. So there would be no need for an MCRN or UNN, as seen in the Expanse series. I'm not so sure. If the former colony begins to compete with the home world for access to resources from the asteroid belt, there is certainly scope for tensions.
The Expanse novels foresee a population of 4-9billion by about the middle of the 23rd century. That also is surprisingly realistic. If we reach a population of 1million by 2050 (ambitious, but possible) then 200 years of population growth at 4.5% per year, results in a population of 6.7billion by 2250.
At first sight, it might appear improbable that we could feed that many people on Mars, given its apparently desolate appearance. But farming based on microalgae, blue-green algae, fungi, aquaculture and C4 land plants, etc, with integrated recycling of micronutrients, could be very productive. Many people find the idea of algae as food unappetising. But as a processed food ingredient, with flavourings added, it could mimic many foods that we are familiar with and be more healthy overall. It roughly 3 times more efficient at converting sunlight photons into food starch, carbohydrates and proteins. So all the food for one person could be grown in a space of a few tens of square metres. A population of 10billion could be fed on a few hundred thousand square kilometers of equatorial Martian land, which is less than half of one percent of Martiansurface area. With abundant fusion energy, indoor (stacked underground) farms are possible as well. So a population rivalling that of Earth is certainly possible.
It seems odd to think of a thriving human civilisation of billions, on a planet where you would be dead in two minutes without an environment suit. That is the greatest gift that technology has bestowed on human beings. It allows us to live almost anywhere. Provided of course,be have a suitable and sufficient energy source.