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tahanson43206,
To be perfectly frank, Void's idea is something that should be pursued first, because if that actually works it means a very simple solution is at hand to travel between planets using bits and pieces of existing flight hardware. I'm not against Void's idea at all, because I don't care how this vehicle gets built as long as it actually works. I'm after the end result, not the aesthetics nor personal preferences. If lopping off the crew compartment of a Starship and welding it up to part of another vehicle actually works, I'll dance a jig over it and move on to the next interesting problem.
tahanson43206,
Why are photovoltaics and wind turbines not being used to build more photovoltaics and wind turbines here on Earth?
Hazard a guess as to why you think that is.
Calliban,
I wrote a rather lengthy comment on that video illustrating a basic math breakdown of Supercritical CO2 gas turbine component masses based upon a real installation here in Texas, and about two days later either the channel owner or YouTube deleted my comment, despite praising the effort he put in and subscribing to his channel.
What I've found is that the people who believe in this electrification of everything silliness are so lost in their fantasy world that when ugly reality is presented to them, they ignore it and try to pretend that reality isn't real. Sadly, physics is not very charitable to ideological beliefs.
In the very first sentence of my comment, I illustrated how the mass of Copper wiring alone would exceed the mass of the entire solar thermal solution based upon sCO2, even if I was "off" by a factor of 2X.
I'm reproducing my comment left on his channel below so that people with basic math skills can see what reality actually looks like:
Photovoltaics require about 5,500kg of Copper per 1MWe of output, or 5,500,000kg per 1GWe, especially low efficiency thin film arrays, especially when the copper wiring will be heated to 121C before we start trying to pump electricity through it. Most Copper wiring ampacity charts only go up to 90C.
Major component mass breakdown for a 50% thermally efficient solar thermal Recuperated Closed-loop Brayton Cycle (RCBC) Supercritical CO2 (sCO2) gas turbine power plant operating at 255bar and 715C:
Commercially available material:
52,872kg for 2,591,726m^2 of 15 micron / 20.4g/m^2 Aluminized mylar collector to generate 2GWth on the lunar surfaceEstimates based upon an actual working sCO2 gas turbine power plant components already built by SWRI and operating in Texas:
6,250kg sCO2 gas turbine rotor, Haynes 282, at 160kW/kg, but 200kW/kg is closer to reality for 50MW to 300MW sCO2 turbines, so I went with a working system component mass from a sCO2 pilot plant that's already making power
25,000kg sCO2 gas turbine rotor and casing, Inconel 740H
31,250kg sCO2 re-compression turbine rotor and casing
368,098kg 316L diffusion bonded printed circuit heat exchanger, at 16.3MWth/m^3Estimate based upon Wright Electric's liquid-cooled plain old Copper and Iron, non-superconducting aircraft electric motor:
62,500kg 1GW high speed electric motor-generator, at 16kW/kgEstimates using NASA high temp space radiator tech info from NTRS:
990,040kg for 20mm ID Haynes 282, at 1.146kg/m, hoop stress is 22.491ksi at 255bar, ~3m of collector area required to generate 715C, I think (may actually be closer to 4m, I just guessed at this based upon a high temp solar thermal receiver tube design built for NREL, and zero flow or thermal-hydraulic analysis to determine if other factors will prevent this from working at all)
250,000kg for Carbon Fibers (not CFRP) vacuum brazed to Inconel 718 (NASA high-temp space radiator for nuclear power), at 600CMass Total: 1,786,010kg
There will be additional masses associated with the mounts for the sCO2 turbine and generator, plumbing, valves, CO2 thermal power transfer fluid, a separate coolant loop to cool the generator, and thermal energy storage materials since most places on the moon have 336 hours of light followed by 336 hours of darkness. Storing 336GWh of electricity in Lithium-ion batteries will also be a mass-related show stopper for thin film photovoltaics, if the batteries are protected to NASA standards. I didn't bother to calculate how many kilos of CO2 are in the loop, either. I could be off by a factor of 2X and a 1GWe solar thermal power plant is still substantially lighter than the mass of Copper wiring required by a 12% efficient 1GWe thin film solar array. The same holds true on Earth. The ERoEI of photovoltaics and wind turbines vs solar thermal is not much of a comparison after plant longevity, all material inputs, and appropriate energy storage devices are considered.
I thought this video was a solid attempt at comparing solar thermal and thin film photovoltaics. NASA uses small Stirling engines for power due to their high reliability without maintenance. Nobody there, or at least nobody that I've ever spoken to, is seriously considering them for large power plants. The radiation environment that the thin film will be subjected to should also be considered. I doubt it lasts longer than 10 years. NREL's solar thermal demonstrator built in the 1970s has already operated for 50 years. Kudos to AnthroFuturism. I love the work he put in. Subscribed.
It's amazing how poorly received plain old energy reality tends to be, but that's because I don't allow ideological beliefs to "control" what I think about real tangible power generating technology.
Source documentation, which I'm more than willing to provide, comes from NREL, SWRI, NASA, and private industry. In my mass estimates, I was very conservative, and based them upon straight linear scale-up of the existing sCO2 pilot power plants which are now operational.
It later turned out, after doing even more reading and listening to test results YouTube videos reported by SWRI, that I overestimated the mass of most sCO2 pilot power plant components, such as the recuperator. They're actually transferring 43MW/m^3 of thermal power through their prototype heat exchangers. That is a stupid amount of power crammed into such tiny components, relative to steam plants. One of the PhDs from SWRI said the power density of the sCO2 turbine is very similar to the high pressure LOX turbopump on the RS-25. What's more, they're designing all the "hot section" components for 100,000hr service lives or greater. Few parts of a RS-25 lives for 100hrs, never mind 100,000hrs. That's why this tech took 20 years to develop. The tiny 16MWth / 10MWe turbine rotor was actually 200kW/kg, not the 160kW/kg I used in my estimate, apparently based upon smaller prototypes from SWRI documentation. That means a scale-up to 50MW to 300MW will deliver greater power density. If they start making components from CMCs, gravimetric power density will further increase by a factor of 3X to 4X with no increase in operating temperature. C/SiC ceramic composites are designed to live at 1,000C to 1,200C, rather than 715C. 600kW/kg is already a crazy power density figure, but sCO2 turbine rotors operating at 1,000C could go as high as 1MW/kg. That is just plain nuts. The reduction gearbox, electric generator, and its base support may very well become the single heaviest component of a 1GWe solar thermal power plant on the moon or Mars.
There are 4X 300MWe power plants being built at 4 different sites here in America by Occidental Petroleum and 8 Rivers Capital (2 are natural gas and 2 are coal-fired and recapture their own CO2 emissions for piping to the fracking industry), with multiple smaller units under construction elsewhere in the US, UK, EU, Russia, India, and China. I think there's one being built in Brazil as well. I didn't check what South Korea and Japan have in the works. The 50MW units are for natural gas pipeline compression and the 300MW units are for commercial electric power.
So far as I'm aware, there is no serious attempt to use Stirling engines for commercial power. We're moving to Recompression Closed-loop Brayton Cycle (natural gas or oil) and Allam-Fetvedt Cycle (coal) power plants, because all of it fits inside of the area occupied by a normal American-sized house.
For the 500 colonist ship, I'm allocating the following masses:
350t - ship's hull
50t - ship's complement
155t - food for 180 days
100t - water reserves
45t - furnishings, clothing, toiletries, and misc consumables
Mangalloy is 7,800kg/m^3, which only provides 44.872m^3 of hull material to work with
Sylramic fiber C/SiC Ceramic Matrix Composite is 3,210kg/m^3, providing 109.034m^3 of hull material
Both materials provide comparable tensile strengths in finished form. CMCs are stiffer than steel, so less deformation under load. The CMC would not lose much strength in the event of a fire aboard ship, as Sylramic fiber was intended to out-perform Nickel-based superalloys. The proposed Mangalloy cannot operate above 260C without losing its ductility over time.
Using CMCs for primary structure would necessitate sealants between the individual "donuts" / "wedges" comprising the toroidal habitation ring structures. This implies use of air-tight gaskets between sections, so perhaps thin stainless steel gas-tight crush seals can be fabricated since these work pretty well in high pressure applications, such as air conditioning systems. Multiple sections would be bolted together and uniformly "crush down" on the sealing gaskets. Silicone seals could also be used, which are standard for US Navy ships, but nowhere near as heat resistant as multi-layer metal gaskets. CMCs may not benefit as much as metals do from ceramic thermal barrier coatings to protect the material from corrosion damage or weakening due to fire, and thermal expansion is markedly lower than it is for metals, but C/SiC's thermal transfer coefficient is or can be at least 2X higher than Mangalloy, so additional thermal insulation is required. The cost issue at play is that for near-zero porosity, as achieved by CMC components like gas turbine blades or hot section casings, some kind of vapor infiltration processing method is required to fully densify the ceramic matrix around the fiber reinforcement, and that process is expensive.
The net benefits of CMCs of the variety considered here are equal strength to austenitic steels (on par or stronger than Mangalloy and meaningfully stronger than stainless), comparable or greater stiffness, much lower CTE, much greater temperature tolerance range from deeply cryogenic to 1,200C, thermal shock resistance, much greater achievable section thicknesses for a given weight, and the potential to either reduce weight or add strength to critical areas. There would be no on-orbit fixturing and welding of the hull structure, merely bolting it together. That would greatly reduce the complexity and cost associated with assembly. We have extensive experience with on-orbit assembly, but very little with on-orbit fabrication. There would be no post-fabrication grinding / machining of the CMCs, either, because they're created using high precision molds. Metal expands and contracts quite a bit after sintering or casting, which implies cleanup machining of some very large individual parts, though not terribly heavy.
There would be a modest radiation dose reduction over steels, but ceramics are still oxidized or nitrided metals at the end of the day, albeit thicker and combined with Oxygen or Nitrogen which promotes more elastic collisions to help absorb ionizing radiation, very strong microwave radiation absorption, decent X-ray radiation absorption. It won't do much of anything against gamma rays or heavy relativistic ions, but neither will thinner sections of steel, which will promote showering of the crew with secondaries. The interior and exterior BNNT fabric overwraps will do a much better job against secondary radiation, but are still basically sheets of typing paper being pitted against armor piercing bullets. Only a large volume of water or other Hydrogen-rich materials have much chance against GCRs. For a 6 month trip, apart from shielding against solar flares and CMEs, I think the rest of the radiation dose has to be "taken on the chin" until active systems are devised to protect ships.
300t of reserve mass will be allocated to:
ship's amenities such as the cafeteria, food cooking and storage, toilets, showers, etc
interior airtight bulkheads and hatches
interior thermal protection fabrics
exterior hull ballistic and thermal protection fabrics
sCO2 gas turbine RTG electrical power supplies
LCO2 storage for RTGs and shipboard firefighting
thin film photovoltaics for supplemental electrical power
radiator arrays for thermal regulation
electrical wiring and air ducts for interior air circulation
docking hatches, fittings and electric motors for counter-rotation
PEMFC main propulsion system power supply
H2O propellant ion engines
compressed H2 / O2 storage tanks to power the main propulsion fuel cell
supplemental water propellant storage tanks
Total dry mass target, less propellant, is 1,000t.
Total wet mass target is 1,500t to 1,700t.
tahanson43206,
I applied the same fix that I applied for the "Fire" style. I just checked the file permissions again. This is either a cache issue or an entirely different problem.
tahanson43206,
Air and Earth styles should work now.
Terraformer,
It's about time somebody started working on this. If we want to do solar and wind power in a way that makes an actual difference to global CO2 emissions, then we're looking at using solar thermal power, mechanical wind turbines, and a surrounding ecosystem of energy storage technologies that don't require quantities of specialty metals we can't realistically obtain.
Capturing and repurposing CO2 emissions into saleable products was always the correct way to address this issue. If recycling is not a dirty word when it comes to metals or plastics, then it shouldn't be looked down upon when it comes to CO2, either.
We've so little to show for the money spent thus far because we pursued academic ideological solutions past the point where technology could keep pace with the rhetoric broadcasted by mass media. Making everything electrical is no longer a technological dead-end when we can source and recycle the specialty metals required, but not a moment before. Thankfully, electrification is not required for reducing or capturing our CO2 emissions, and may be an impediment in some cases.
What I've proposed is still a "wind and solar" solution at the end of the day, so it would be nice if the people advocating for "wind and solar" took a hard-nosed look at what we can do using what we can actually make in the volumes required to put a measurable dent in the overall problem. We're going to progress a lot faster by pursuing scalable solutions with a low entry bar, technologically speaking.
tahanson43206,
My final thoughts on Void's proposal is that if the required changes prove to be relatively minor, then it could be a faster / cheaper pathway towards initial human Mars exploration missions. By its very nature, it will never be a like-kind substitute for a purpose-built highly compartmentalized ship intended for transporting hundreds of colonists vs a dozen astronauts.
I would place Void's proposal in its own AG-enabled Large Ship Prototype category. It could be used to prove the feasibility of AG and counter-rotation, evaluate the effectiveness of the various protection schemes afforded to a large interplanetary transport ship, and function as a testbed for the life support / power / propulsion systems, as well as the first operational use of an interplanetary transport ship worthy of that title.
tahanson43206,
If you're thinking that certain parts of a Starship can be treated like "Legos", then I would say that's probably not going to happen. Starship is the upper stage of a launch vehicle, so that's what it was optimized to be. Skylab was an extensively modified upper stage that was built on the ground in a fab facility. Redesign of the existing hull structure is likely required to ensure it's structurally sound for the intended use as an orbital habitation module providing artificial gravity over long periods of time.
What parts of a Starship crew compartment will require structural reinforcement as part of a new artificial gravity orbital habitation module design?
Those changes could be relatively minor, yet will likely be significant, in much the same way that strapping two boosters to the side of a Falcon 9 first stage amounted to a complete redesign of the core stage, such that it shared virtually nothing in common, structurally speaking, with an actual Falcon 9 booster stage. The forces exerted won't be nearly as extreme as a pair of strap-on booster stages, but the load path and reinforcement wlll change from how Starship was previously designed. If doing that proves relatively simple and easy, then it's a happy accident.
Why not just start from scratch with a vehicle design optimized for the intended use case?
Starship uses very weak and therefore heavy (for the strength provided) stainless steel. I'm talking about working with a material that's 2X to 3X stronger, because this vehicle will be at least as heavy as a fully fueled Starship while providing far more pressurized volume to make it both comfortable and well-protected for long duration missions.
Assume for a moment that since you no longer have any support structure beneath that pressurized compartment, that you'll require significant alterations. If you're doing that on the ground, then that portion of the vehicle is flying to orbit in that configuration. We've changed the outer mold line of a hypersonic vehicle, and then we're going to detach it from the propellant tanks on-orbit unless we're doing the "spinning baton" design with a complete Starship. If we don't detach the propellant tanks and engines, then we're hauling around 100t of dead mass which must be resisted by the structure connecting the pair of Starships.
Could that be done relatively easily on-orbit?
I honestly don't know, but I suspect we're looking at a significant vehicle redesign of Starship.
If we're going to go to that trouble to repurpose a portion of the existing flight vehicle design, then why not design a new vehicle from scratch to get all of the features we really want?
High-Manganese steel is an acceptable substitute for 316L stainless when the atmosphere of the interior of the ship, and thus the metal hull, will be kept relatively warm.
Weldable 316L austenitic stainless yields at 25ksi. Non-weldable 316 stainless yields at 30ksi.
Weldable austenitic Mangalloy yields between 50ksi to 75ksi.
At least doubling both yield strength and hardness over 316, as well as substantially increased abrasion resistance if objects ever impact the interior of the hull by accident, is very important. At room temperatures, Mangalloy steels will have ductility comparable to austenitic stainless steels, but at a minor fraction of the cost. 316 will have better ductility at deeply cryogenic temperatures, but I don't think a crewed vehicle with a cryogenically cold hull is compatible with human survival. Thermal conduction, in conjunction with a multi-layered insulation and ballistic protection overwrap applied to the hull's exterior, should ensure that no part of the hull is subjected to the greatest extremes of hot or cold.
This is a very lengthy but very expressive missive on all aspects of high-Managanese steel production and fabrication processes, with comparisons made with austenitic stainless steels as well as other kinds of steels and some insight as to why to choose one over the other:
Austenitic Manganese Steel
I would fabricate the hull from Mangalloy, with a keen eye towards the weldability of the alloy without cracking or stress concentration, then I would coat the entire hull, inside and out, with a plasma spray deposited ceramic coating to resist corrosion damage, and then I would apply a CNT fabric overwrap that provides both ballistic protection and acts as a "heat spreader" to maintain temperature uniformity over the entire hull. Very large rolls of CNT fabric "matting", similar to unidirectional Carbon Fiber tapes, are now available. On the interior, I would apply BNNT fabric to the hull, to absorb secondary radiation, act as a thermal blanket, and prevent an interior fire from weakening the steel or otherwise threatening the airtight integrity of the hull.
To keep weight reasonable, we're talking about using rather thin pieces of sheet steel, hence the use of a stronger base metal and the elaborate protection scheme afforded to the ship's crew and passengers.
Wiring for shipboard electrical systems would consist of CNT conductors with BNNT fabric insulators (not plastic). This will drastically reduce weight over shielded Copper conductors and plastic insulation, by about 80%, increase the resistance of the wiring strands to cutting or abrasion, provide extreme resistance to fire, and reduce the possibility of a fire generating toxic smoke in the cabin air supply. The electrical connectors will use BNNT-reinforced sintered ceramics for fire resistance and weight reduction. Here again, the elaborate protection scheme is centered around preventing fires, fire resistance, and general durability. The reduction in interior metal content is also driven by a desire to limit secondary radiation emission associated with high energy particles (galactic cosmic rays) striking the hull.
I think the most economic way to produce the ship's hull will be using a series of precision castings that have been ground to final size. The reason for this has to do with achieving near-perfect balance of all parts of the rotating assemblies.
Whereas modern gas turbine blades are hollow to circulate cooling air through the internal channels depicted above, we require an active stabilization system that keeps the rotating components balanced as weight shifts around inside the ship. Apart from preventing unwanted changes to the ship's trajectory, the primary reason for doing this is preventing uneven wear on bearings or distribution of force on highly loaded thin-walled components.
This vessel is an aerospace vehicle, not an ocean-going ship in the conventional sense. Weight matters quite a lot, as does the quality of the materials used and workmanship. We need to be very deliberate about how we go about approaching its design, not fixating on any single aspect of the vehicle to the detriment of all others, and we must remain pragmatic about what the vehicle is optimized to do.
After reviewing state-of-the-art PEMFC and ion engine technology, with PEMFCs fast approaching 40kW/kg, I no longer think we need nuclear propulsion. This moves the large ship concept solidly into the realm of feasibility, because there are now water propellant ion engines generating sufficient thrust and Isp. We still need about 500MWe, meaning a 12,500kg fuel cell, but we're going to use a novel application of the steam being generated by the fuel cell. We're going to push the fuel byproduct (steam) required to power the fuel cell, through the ion engines. To my knowledge, this has never been done before, but we're going to do it, because we need to repurpose that which powers the fuel cell to also supply reaction mass to the ion engines.
We may still require nuclear power to provide sufficient life support electrical power for 500 colonists, but that which powers the propulsion energy generating system and the propellant itself can now be the same materials. Rather than using cryogens, we now have high pressure CFRP storage tanks that can store sufficient Oxygen and Hydrogen. From my reading of the literature on Mangalloy steel, special formulations of that material do not appear to suffer from Hydrogen permeation and embrittlement to nearly the same degree as other metals such as stainless steel, which means we can use steel liners for the Hydrogen storage tanks. Oxygen presents a real challenge for Mangalloy, which means the CFRP Oxygen tanks will require stainless liners or Mangalloy with an appropriate coating. We may still use cryogens and light metal tanks for achieving escape velocity from Earth, but the return trip will rely upon a lesser volume of highly compressed gas.
The greater use we make of non-nuclear COTS technology, the greater our chances of convincing an organization such as SpaceX to build purpose-built interplanetary transport ships and landers, keeping those valuable Starships here at Earth, for economic delivery of payloads to LEO. We may be able to achieve better results using nuclear technologies, but the licensing and economic hurdles to implementation are extreme. We will certainly need fission surface power systems for colonization, so perhaps that's where political and monetary capital should be expended to bring this dream to fruition.
This is the basic shape for the large ship habitation ring:
Whether this "habitation wheel" depicted above uses 3, 4, 5, 6, or even more spokes to support the forces acting upon it is less relevant than the fact that you have two of these habitation wheels rotating in opposite directions so that the forces exerted on the vehicle cancel each other out, and thus a gyroscopically stable vehicle design is achieved. A "stable vehicle" is one that does not precess perpendicular to the axis of rotation and travel, the way a rifle bullet does. This is very important for both trajectory computation and thrusting in the direction of intended travel. Not having to compensate for the vehicle's rotation in one plane causing it to slowly yaw in another plane, and thus "drift" off-course, is very important. If the axis of rotation and the direction of intended travel is in the X-plane, similarly to a rifle bullet, then the vehicle is affected by a yaw in the Y-plane. As it pertains to actual bullets, the slang term for this unwanted behavior is "spin drift". This is a very real phenomenon, and over great distances it has a very substantial effect on trajectory. If bullets had two parts with equal mass rotating in opposite directions, then this would not need to be accounted for in ballistics computations.
Over 193.75 million miles, spin drift would affect the vehicle's trajectory by about 64,583 statute miles. That is a very significant deviation, considering the fact that Mars has a diameter of 4,212 miles. You would "miss" the planet Mars entirely if you failed to account for a deviation of that magnitude. You obviously could compensate, but this seems like a needless complication since it's affecting the vehicle at all times while it's rotating, and will in fact affect where the "nose" is pointing, thus the direction of thrusting. Using counter-rotation to stabilize the trajectory of a vehicle providing artificial gravity for its crew means whatever direction you point the vehicle in, you need only account for gravitational fields from large bodies and the fundamentals of orbital mechanics when plotting intercepts to distant planets.
Edit:
The following link goes to a Physics Forums discussion where using counter-rotation to side-step this problem is being discussed. On that forum, just as we already did during one of our Zoom sessions, and I actually wrote some simplistic software to do, the people posting in the topic are telling the OP to make sure he / she accounts for Mass Moment of Inertia. I believe we did that to determine that magnitude of the force applied to the vehicle, but in the OP's application it matters to the accuracy of the gyro-stabilized flight control computer.
tahanson43206,
After I log in, I still see the stylesheets applied to all the web pages. I poked around through a lot of the different pages and menu options.
tahanson43206,
I fixed the stylesheets on the "new" NewMars forums.
1bbl of crude = 139.3kg
Carbon = 127.6kg (468kg CO2)
Hydrogen = 11.6kg
1kg CO2 (direct ocean capture) = 1.8kWh
1kg H2 (water electrolysis) = 50kWh
CO2 = 842.4kWh/bbl
H2 = 580kWh/bbl
Sabatier reaction = 4,637.3kWh/139.3kg
Input Insolation = 6.85kWh/m^2/day (in a Midwest desert)
Polished Aluminum Mirror = 6.165kWh/m^2/day
6,059.7kWh / 6.165Wh/m^2/day = 983m^2 of solar thermal collector area per bbl per day
20,246,575bbl/day * 983m^2/bbl/day = 19,902,383,225m^2 = 19,903km^2 (141km by 141km)
2mm x 1m x 1m = 34.5394lbs/m^2 of rolled / stamped steel (hot-dipped in Aluminum, then polished)
19,902,383,225m^2 * 34.5394lbs/m^2 = 687,416,375,162lbs / 311,807,194t
$880/t * 311,807,194t = $274,390,330,720
Let’s double that figure to $550B to account for the steel support structure for the solar thermal mirrors.
Crude currently sells for about $67/bbl.
$67/bbl * 7,390,000,000bbl/year = $495B
Let’s double the cost again to account for fabrication and installation labor. We’re sitting at around $1T.
Over 20 years, we’re spending around $50B/year to supply our hydrocarbon energy input requirements for the next century.
3.11Bt of steel produces sufficient energy input for global supply of petroleum of petroleum base product (Methane). We produce about 1.85Bt of steel per year, so the materials input to supply the petroleum base product for at least the next human lifetime is equivalent to 2 years of steel production. We'll have to add more equipment and energy to go from Methane to gasoline or diesel, but after you produce the Methane, the input energy requirements to go from Methane to gasoline are not nearly so high.
Almost anyone with a pocket calculator could quickly and easily figure out that not running out of energy is dramatically more important than the paltry amount of money and steel required to ensure that never happens. It's nuts (to me) that an oil company hasn't already determined that making sure the profits never stop rolling in is the absolute best reason to recycle CO2. If there are energy surpluses to be had, then we make sure we capture extra CO2 and convert that to solid Carbon ("coal") using Gallium.
No tire company functions without Carbon Black. No coal-fired power plant functions without coal. No Carbon Fiber company functions without Carbon. None of our advanced manufacturing tech, or not-so-advanced tech, functions at all without on-demand energy. That is a fact, no matter how much we attempt to ignore reality.
An actual synthetic petroleum production facility is at least guaranteed to produce the goods. Another oil well may or may not, and it won't produce for very long since we've already consumed the easy-to-get oil.
It seems as if we need some long-term thinking here.
US 2024 Elections Results Updates
House Elections Results
Republicans secured 218 seats.
Democrats secured 212 seats.
These are official results reported by The Associated Press.
There is one more Republican voting district in California which has not been called. None of the House election results from Alaska have been certified now, either, but the Republicans have a 55% to 40% advantage over the Democrats. I'm guessing they're recounting the votes in Alaska, for whatever reason. Either way, the Republicans will have a majority in the House, as-is, and only the number of seats in the majority remains unknown.
The Republican Party has won the Presidency, a majority in the Senate, a majority in the House, the popular vote, and a majority of the US states have elected Republican governors.
I'm not sure how much clearer the message needs to be for our representatives to, you know, represent our interests in government, as opposed to the interests of tiny minority groups within the Democrat Party. It's time to change course by trying something we barely pay lip service to these days- using the power of government to at least attempt to give people a better future. We cannot do that through the politics of group identity and selfishness. It's time to refocus on the basics of running a country properly, which has not happened during the past four years under a President deemed so senile by his own party that he was judged to be incapable of leading or merely running for office. His Vice President was so deeply unpopular with her own party that she did not receive a single nomination vote for President during her bid during the 2020 Presidential election.
The majority of Americans have spoken by casting their votes. They want to take a different course of action.
Do we have the attention of BOTH political parties yet?
Is anyone from the Democrat Party or Republican Party actually listening to us?
The way we became a nation in decline was by allowing the shallow self-interested people running it to pander to special interests.
We want a better economic future to look forward to, not worse. We need jobs for our own people and inflation that doesn't crush the average worker. I don't care if rich people get richer, so long as all the poor and middle class people also get richer. I don't look down my nose at rich or poor people, but I want a better outcome for as many people as we can possibly give opportunities to. Some will win. Some will lose. Equality of outcome is either impossible or insanity. Nothing will ever be 100% equal for everyone everywhere, unless we're all dead set on becoming equally poor and destitute. Communists are always ready and willing to deliver oblivion, if that is what people truly want. They always think they're smarter than the last group, and in due time they're always proven wrong, without exception. Lusting after what your neighbor has is a societal dead end. I want American society to continue on, long after I'm gone.
We're not looking for handouts from the government, merely opportunities. We don't view the government as our saviors or our piggy bank. We wish that other people would stop viewing both the government AND their fellow citizens this way. Rich people cannot give you everything you could possibly want, even if you took every last cent they had. Similarly, rich people need to learn that squeezing every last cent out of the poor is equally asinine. The least well off amongst my fellow Americans hold a higher station in life than the kings and queens of antiquity.
Government is NOT supposed to hand out "free stuff" to some special group of political supporters. The purpose of government is to use force to achieve agreed-upon objectives. It's not "pretty" scalpel which can perform plastic surgery on society to remake society into a beautiful utopia. Government is a blood-stained broadsword covered with dents and nicks in the blade from all the skulls it has cleaved from the bodies of its victims. Government is not something to be propped up on a pedestal. Government is something you use as a final resort, when nothing else gets the job done.
We want the welfare of our own fellow Americans treated with at least as much importance as that of foreigners who merely crossed our borders illegally. There can be no legitimacy through mere declaration or ignoring our existing laws whenever they run afoul of party politics.
We want violent career criminals locked up, not coddled or allowed to run wild in our streets. Nobody here deliberately "voted for that", and most felons cannot vote, so the people who haven't raped, robbed, or murdered their fellow citizens deserve at least as much deference as those who have, and perhaps a lot more.
We want a Department of Defense that either lives up to that name, or is correctly rebranded as a "Department of Offense". There's no "defending" going on when we're actively looking to start new wars. War is supposed to be the final option, not the "go-to" option. Foreign policy involves diplomacy. When are we going to start practicing that again? For those who don't know, diplomacy is the art of telling someone to go to hell in such a way that they look forward to the journey. We need more of that and less murdering each other to take what the other has or in response to some petty grievance.
America is a deeply religious country. Some of our faithful follow the religion of money or science or government itself, others follow the edicts of their "God" (whichever one that happens to be), and the rest I really have no idea about most of the time. America was founded on freedom OF religion, not freedom FROM religion.
Nobody has all the answers. Anyone who claims to is obviously lying. Sometimes we can fall back on things that we know worked well, but other times not so much. On the go forward, I'm hoping that we start seeking answers to the big questions, together. If there's no debate and no questioning, then there's no learning, either. We cannot get to this "better future", unless we do so together. It's going to be messy and uncertain. At times, it will seem dangerous and scary. Unlike slavery, freedom doesn't come with a list of guarantees, and it absolutely is not free. We have to fight for it, and for each other, or there is no future worth living for us or anyone else. Nobody is coming to save us. We are the cavalry.
I think that SSTO I proposed would make a fantastic upper stage for the Super Heavy booster. It generates lift, so it has cross-range and can land on a runway. The pressurized passenger compartment could be used to return ZBLAN fiber optic cable from orbit, back to Earth, with a lower probability of loss than a vertically landed upper stage. The fiber optic cable cargo would be much easier to offload than it would be from Starship, and the crew could oversee the loading and unloading of the cargo. The upper stage could then be flown back to the launch pad using a conventional jet engine, for which there's plenty of mass margin since it doesn't need to achieve orbit all on its own. The booster provides enough of a Delta-V reduction that the vehicle could achieve high orbit to drop off passengers, come back down to a lower orbital altitude to pick up ZBLAN from the manufacturing plant, and then return to Earth, and to choose where to land to offload the cargo. It could go to Silicon Valley, Japan, South Korea, or anywhere else that a paying customer wants the latest and greatest fiber optics tech for their networks, which would probably be anywhere with a runway capable of landing an airliner.
Passengers could go up to an awaiting interplanetary transport for the lucky few who get selected to venture out to our colonies, the vehicle reduces its orbital altitude to stop by an orbital manufacturing facility to pick up fiber optics or photonics "chips" or similarly valuable products, and then the high value cargo and any returning passengers reenter and fly to an airport of convenience (for delivery of the cargo) here on Earth. The passengers then fly back to the states or wherever they're originally from, aboard a commercial airliner. There are revenue generating payloads going both ways, so the ticket price to go to another planet could be reduced since some of the generated revenue comes from the passengers and the rest comes from high-cost / high-demand electronics and telecommunications products that we'd very much like to use to replace existing Copper or lesser quality fiber optics here on Earth, but unfortunately the ZBLAN crystals grown on Earth look like crap, whereas ones grown in orbit look flawless.
This would be the first practical application of space, used to simultaneously unlock interplanetary transport and orbital manufacturing of next generation computers and communications equipment. The photonics-based computing and sensor tech would dramatically reduce the energy consumption associated with data center computing and AI, which is now eating more energy than the entire global air travel industry. Low cost fully reusable rockets are akin to a "cheat code" to level-up our tech and travel capabilities. There's an implicit defense application for Space Force as well. If we can use some of the interplanetary transport tech to go after the metals in the main belt, then we get functionally unlimited Platinum group metal catalysts for advanced energy tech, CO2 removal, and various other technological "goodies". Beyond that, we need to find new sources of Copper and Silver, or this idea of electrifying everything will remain a dream forever.
Our newly formed "Department of Government Efficiency" should appreciate the "How many different birds can we kill with the same stone?" aspect of this as well. We have lots of people with degrees, and we just imported millions of people with hand labor skills but no degrees. Unfortunately for both groups, there are few jobs worth doing because they don't ultimately take us anywhere new. Solving these engineering-based problems, none of which are beyond our technical capabilities so they need not devolve into endless pointless science experiments, would be well worth the time and labor devoted to it.
I think WWIII is already in-progress, even if it remains undeclared, but this "unlock space" project would become the "silver lining" following the hell on Earth that we're about to be subjected to. Our children can look forward to this on the other side of the war- something which puts those of us who remain onto a project that is broadly beneficial to humanity, and provides a huge surge in demand for people, ideas, materials, and technologies. The Greatest Generation had the opportunity to "remake the world" following WWII. Our children will get the same opportunity. Everything involving humanity operates over cycles. Along the way, we somehow manage to progress a bit.
US 2024 Elections Results Updates
House Elections Results
Republicans secured 217 seats.
Democrats secured 207 seats.
These are official results reported by The Associated Press.
Total reported results look much better now for the West Coast states, with vote tabulation nearing 90% completed. The popular vote margin currently stands at just over 3.1 million votes in favor of President-elect Trump. The vote breakdown amongst the West Coast states is around 60% in favor of Vice President Harris, 40% in favor of President-elect Trump. Vote allocation appears closer for the two candidates in the Midwest and East Coast states, with Massachusetts, Maryland, and District of Columbia being the only exceptions.
Calliban,
I'm going off of reporting from various left and right foreign and domestic media reports that they're not going to certify election results until the end of this week, but that the Republicans have now gained the votes to secure 219 seats and the Democrats gained or likely will gain the votes required to secure 213 seats. By current vote tally, Republicans have 219 seats and Democrats have 210 seats. The 3 seat discrepancy is expected to go to the Democrat candidates.
If that changes between now and the end of the week, I'll add an update. The remaining races are either too close to call or contested by the candidates because the results are close enough to request recounts. That means there will be a handful of races which require recounts, but 432 of 435 seats appear to be accounted for at the time I wrote my last post. If nothing unusual happens between now and then, the most probable makeup of the House of Congress going into 2025, will include 219 Republicans and 213 Democrats.
"270toWin" reports the results before they're certified. The Associated Press remains the official reporter of election results, but again, they typically only report results after results are certified. Based purely on counted votes and majorities, the 219 Republicans and 213 Democrats appears to be the most probable outcome.
US 2024 Elections Results Updates
House Elections Results
Republicans secured 218 seats!
For whatever reason, The Associated Press is still behind the power curve in timely reporting of results, but Reuters, The Hill, and a handful of other media agencies are now reporting that the Republican Party has secured 218 seats in the House.
270towin.com - Republicans Retain House Majority - By 270toWin Staff - November 11, 2024, 8:05 PM ET
Monday evening, AZ-06 was called for Republican Juan Ciscomani, who was reelected for a second term. That win gives the GOP 218 seats, ensuring they will retain their majority when the 119th Congress begins in January.
Earlier in the day, CO-08 was called for Republican Gabe Evans, who defeated freshman Democrat Yadira Caraveo.
Eight House races remain uncalled. Seven are in California, one in Alaska.
In California, Tuesday is the final day for ballots to arrive and be counted, assuming they were postmarked by Election Day. The state is very slow at counting (this is not new), so it is unclear when those races will be called.
In Alaska, there probably won't be a race call until the ranked choice tabulation on November 20.
The Republicans appear to have won the Presidency, the Senate, the House, and the popular vote.
I think this headline speaks for itself:
A Federal Emergency Management Agency employee has been fired after they advised their disaster relief team to avoid homes with signs supporting former President Donald Trump while canvassing in Florida in the aftermath of Hurricane Milton, the agency’s administrator said Saturday.
FEMA Administrator Deanne Criswell called the actions of the employee "reprehensible" and said they have been terminated from their role.
These political clowns actually wrote in their official government records, "Trump sign, no entry per leadership. Implement best practices, avoid homes advertising Trump."
FEMA states that this incident in Florida is believed to be an isolated incident, but weaponization of politics aptly explains why FEMA and local officials did not help residents living in Appalachia in the wake of Hurricane Helene, and actively prevented private citizens from other parts of the country from bringing in disaster relief supplies (food, bottled water, and blankets) using personal helicopters and high water pickup trucks, as well as threatening these volunteers with arrest if they continued helping those living there. Thankfully, some of these civilian first responders ignored the government's threats to arrest them and continued bringing in supplies.
I would opine that perhaps "FEMA" ("Federal Emergency Management Agency") should change it's name to "DEMA" ("Democrat Emergency Management Agency") if those working within FEMA only wish to provide disaster relief to Democrats, and that funding "DEMA" be considered optional for all Republicans. Maybe Elon Musk's new Government Efficiency Agency can cut FEMA's funding to only whatever is required to serve Democrats. Assuming Democrats don't attempt to arrest civilians providing disaster relief, Republicans can rely upon private citizens with religious core values (love for your fellow citizens, willingness to serve and to sacrifice for others, and the ability to look past political beliefs) to provide disaster relief whilst Democrats are free to spend money on other Democrats, or not, however they see fit.
This is exactly what I meant when I admonished Democrats to "stop pouring acid on the fabric of society". There can be no trust between government and the citizenry if those in government are using the power of government as a cudgel against their political opponents. Either tell your fellow Democrats to cut this crap out, or expect big changes to government in the near future. If half of the people in government only want government to serve those aligned with their partisan politics, then that is what government will become. At that point, you will no longer have the consent of the governed, for at least half the population. Since all legitimate forms of government are derived from the consent of the governed, we will rapidly cease to have a functioning government.
In the two days since President-elect Trump was elected as President, the following events have taken place:
1. Mexico's President has announced that she's going to start turning back the migrant caravans and force them to remain in place and wait their turn to immigrate into America the legal way.
2. Palestine's Hamas has requested an end to the war with Israel.
3. Yemen's Houthis have requested a cease fire.
4. Russia's President has requested a meeting with President-elect Trump to end the war in Ukraine.
5. Steve Madden executives have announced plans to cut manufacturing in China by half in the coming months, and will discuss making their apparel and fashion accessories in America.
6. Democrats in New York and California have announced that they intend to continue the legal warfare against President Trump while the US Department of Justice has been directed to halt all legal actions against the President-elect.
I sure hope all that suffering, death, and destruction to enrich the privileged few was worth it.
President-elect Trump should focus exclusively on:
1. Fixing the American economic issues related to energy extraction and domestic manufacturing
2. Border control and illegal immigration issue allowing violent criminals to enter America and prey upon Americans and other illegals
3. Foreign wars and antagonistic relationships with our adversaries, namely China, Russia, and Iran
As someone who actually voted for President-elect Trump, I listened intently when he promised to do those three things and nothing else, in his victory speech. I expect him to remain faithful to his word, or he no longer has my support. The Republican Party only has the most tenuous of support from me, presuming they work with President-elect Trump to deliver on his promises. If the man I voted for does those things and nothing else, then his presidency will be a breath of fresh air when compared to the petty self-serving behavior of President Biden's administration.
I am completely onboard with America focusing on fixing our own numerous and varied domestic problems, which have strained ordinary Americans to the breaking point. Specifically, I want domestic energy and manufacturing output to increase to increase wages, and to help pay down our absurd level of national debt.
I am completely onboard with America refraining from all forms of military adventurism. I want a strong military with thorough realistic training, appropriate tools, and no attempt to "gold plate" our military equipment or capabilities. I do not want our military used to preemptively attack other nations, even if I vehemently disagree with what they're doing. I do not want our intelligence agencies instigating foreign wars. I do not want our military used to support the foreign economic interests of businesses. America should never go to war because some yahoos in an intelligence agency are having a "war fantasy" or XYZ Corporation stands to make a handsome profit from that war.
I am NOT onboard with any ill-advised attempts at "revenge" against political opponents, as the Democrats have engaged in since President Trump was elected in 2016.
I am NOT onboard with indiscriminately bombing the piss out of Palestinian civilians who have guns pointed at them from both Hamas or Hezbollah or Iranian terrorists and Israeli troops. I DO support Israel's right to exist, right to defend their borders, and right to kill all murdering invaders.
I am NOT onboard with spending endless money on killing Russians. I DO support Ukraine's right to exist, right to defend their borders, and right to kill all murdering invaders. I would like them to focus on driving the Russians out of Ukraine, rather than attacking and invading Russia. President Zelensky has said he wants all territory taken from Ukraine, returned to Ukraine. Great. I agree with that 100%, so I would like him to focus on doing that. Invading Russia is not helping to drive the Russians out of Ukraine. It is weakening Ukraine's ability to fight against Russian troops inside Ukraine, because that's how basic math and logic works.
As allies, if Israel or Ukraine or Taiwan or South Korea need to be defended against foreign aggressors, then we send our own military, our own sons and daughters, to fight on their behalf. We articulate why it's necessary to do so to the American people. We commit ourselves to doing only that which is necessary and justifiable. That is what a true ally would do to support their allies. If our allies no longer wish to have American troops on their soil, or refuse to spend agreed upon money for their own defense, then we leave. We don't dictate policy to them, but we both honor the terms of our agreements, or we're no longer behaving as good allies.
Finally, I want American citizens prioritized over immigrants, especially illegal immigrants. All the foreign criminals allowed to pour into America because the officials from President Biden's administration, specifically Secretary Mayorkas, couldn't be bothered to check IDs at the border, is completely unforgivable. Democrats seem to think any immigration laws they disagree with are mere suggestions, rather than codified law. Congress doesn't make suggestions. Congress makes law. The majority of Americans disagree with the Democrats on this point. We would prefer that our elected officials and their political appointees either enforce our laws or work with Congress to change the laws if they think our existing immigration laws are unfair or unenforceable. Maybe our immigration laws could be better, but since we've never made any serious attempts to improve them, we don't actually know, because we haven't tried.
A couple of new classes of materials are under active development for various types of radiation shielding.
The first is CNT or BNNT or Aramid fibers coated with Tungsten. These materails are highly effective at blocking both neutron radiation and gamma rays, as well as secondary gamma rays, with far less mass than traditional or conventional layered High-Z / Low-Z materials such as Lead or Tungsten or Depleted Uranium and a Hydrogen-rich material such as H2O, BeO, plastics, rubbers, and oils. Tests indicate about 90% of the effectiveness of Lead, in terms of shielding against neutrons and gamma rays, at approximately 45% the mass / weight of Lead. This equates to slightly greater mass than Titanium with the net effectiveness of Lead shielding. That is very impressive performance. Polymerized aerogel foams loaded with Tungsten powder are also being evaluated. This kind of radiation shielding is critical for reducing the substantial mass of Tungsten or Lead shadow shielding for nuclear reactors and nuclear rocket engines. The shield can be a flexible fabric or a composite. While the fabric or composite would be much thicker than pure Lead for equal halving thickness, it's also far lighter, far stiffer if it's a rigid composite structure. Thus, these functionalized W-BNNT composites could potentially act as load bearing structural components instead of pure dead weight. Such advanced tech potentially kills three birds with one stone- absorbing neutron leakage, absorbing both primary (releases from fission) and secondary (bremsstrahlung) gamma emissions, and supporting the mass of a heavy reactor core (bearing g-loads associated with launch) or behaving as a de-facto thrust structure for a nuclear rocket engine.
The second class of material combines rare Earth metals / ceramics, such as Samarium Oxide, with Boron and/or polymer binder. These materials are apparently quite effective at stopping neutrons, ions (alphas), and electrons (beta), as well as lower energy X-rays and gamma rays. I suspect this class of material is more useful for stopping the radiation associated with coronal mass ejections and solar flares.
US 2024 Elections Results Updates
House Elections Results
Republicans secured 211 seats.
Democrats secured 199 seats.
US 2024 Elections Results Updates
Presidency Election Results
I'm taking my official election information from The Associated Press, but apparently more than 95% of the vote is now in for Arizona and Nevada, which has yet to be reflected in the vote totals displayed by The Associated Press for whatever reason. However, a number of other news organizations have now called Arizona and Nevada for President-elect Trump. This puts President-elect Trump's Electoral College vote total at 312. We're much closer to having our vote tallies being finalized at this point, with the exception of House races and some local elections.
Presidency election results are not completely finalized, but won't change in a meaningful way.
President-elect Donald J. Trump will become the 47th President of the United States of America.
The 46th President of the United States of America, President Joseph R. Biden Jr, has announced by way of press announcement that a peaceful and orderly transition of power will take place. Our current President has invited President-elect Donald J. Trump to the White House to begin that process.
Senate Elections Results
Republicans secured 53 seats.
Democrats secured 45 seats.
Independents secured 2 seats.
There are at most 1 to 2 Senate seats still being contested. I believe these will go to the Democrats, but outstanding votes remain to be counted in Arizona and Nevada. There is something amiss with their elections process. Both of those states consistently fail to count their votes in a reasonable amount of time.
House Elections Results
Republicans secured 211 seats.
Democrats secured 197 seats.
House race election results are also still being tabulated in Arizona and Nevada.
Gubernatorial Elections Results
Gubernatorial election results appear to be finalized. No changes or challenges are expected.
To the best of my knowledge, no national level ballot measures were set before the American people on which to cast their votes.
To the best of my knowledge, no recounts have been requested at this time, although that may change in the future.
We are very close to achieving a quorum, for the purpose of continuing our form of government and way of life.
I would like to express a heart-felt "thank you" to my fellow Americans who participated in our 2024 elections process. Our form of government, a Constitutional Republic with democratically-elected representatives, functions best when we maximize our participation as citizens of the United States of America- land of the free, home of the brave.