I suspect without ISRU production of bulk orbit sheet metal, the most feasible solution is to repurpose rockets in their whole.
Building a station this large is gonna be costly even within the cargo hold of starship. But six of them, gutted of insides as welded end to end could provide the vast majority of the bulk mass.
This assume rather sophisticated orbital welding and object manipulation; but its feasible we could do it with robots.
> The engines are part of the orbiter, so they can be brought home and reused. The solid boosters drop off minutes after liftoff and are recovered for refurbishment. Even the unmanned heavy-lift cargo launchers use the same basic system. But until our group came along, the huge external tanks were simply dumped, after fueling the shuttle to almost orbital velocity.
> [...] The main purpose of the design is simply to keep the tanks from falling. The two massive ends of the Farm act like a dipole in the gradient of the Earth's gravitational field, so each deck winds up orbiting edge-forward, like a flat plate skimming. This reduces the drag caused by the upper fringes of the atmosphere, extending our orbital lifetime.
I never understand why the rotating station concepts seem to all have rigid tethers, either in the form of a central boom or a rigid circular structure. It would seem like you could get a much larger diameter, so less rotational velocity and more comfort, by attaching rigid, or inflatable in this case, structures with a tether. Compressive loads are non existent, you just need to resist tensile loads.
There are compressive forces. If mass inside the ring is not balanced, it can drag the ring into an ellipsoid. The inner sides of the ellipse are compressed.
A rigid ring can resist some of this inherently, but a rigid spoke to the hub cleanly takes up all the inward forces.
If your ring is not rigid, any perturbations can cause oscillations that throw the whole thing out of balance. Like a gas leak in one compartment adding thrust at a weird angle. Soon the whole ring will be oscillating along its plane, which is obviously bad. You can actively correct with thrusters on each segment, but that's a lot of extra complexity.
Basically it's all about stability. A big rigid object is much harder to shake apart. A metal circle will stay a circle in a lot more circumstances than a circle of rope will. Doubly so when rotating in zero gravity.
Flexible tethers are mainly good for small scale. Swinging a crew capsule about a big mass (Project Hail Mary, Stardancer) is indeed cheap and easy. With the complication that you must completely spin down to maneuver or dock.
I don't think your reasoning here is correct. Take a bicycle wheel for example. The spokes on a bicycle wheel do not take any compressive forces due to the way they are attached to the rim, and yet bicycle wheels can take surprising compressive loads without going oblong.
Maybe I'll go ask the AI oracle, it's only slightly fallible
Or
Maybe I'll go poke an ML model a few different ways to see if it emits interesting word sequences, that I'll then fact-check and study to develop real, deep knowledge.
I'm actually optimistic we can increase the second one, but it requires everyone to help educate our less-technical friends, family, and colleagues.
This isn't new. It's the same person who used to say "but Google said...!" This is a solvable education problem, because we've solved it before.
When its such for my personal edification and idle wonderings, usually the former. If its something that is any way critical to a meaningful decision or something I'm going to publicly share, its the latter.
If it had been solved before we would not be in the predicament we are now, i.e. people might be able to learn but that doesn't mean everyone does. In fact, most do not because we are too busy figuring out how to die leading less fulfilling, more angst-ridden lives.
This is a really nice article that covers the history of space habitats, but it also made me realize that the future of habitable structures has questionable value outside of space tourism.
We have entered an age where humanoid robots are beginning to do many tasks that we thought were exclusively in our domain. At our current pace, I expect they will be able to outperform us in most work settings within a decade or two.
As those robots scale up in their capabilities and numbers, we will send up a fleet of them to space to do the work there. They are far more suited for the environment than humans, and the cost savings would be huge.
The Bigelow stuff was very promising and showed that it could work. The larger units on extruded spokes was a viable path to a .5G space station. This would be doable with three (possibly 4) Starship launches[1].
[1] Caveat Starship has to reach its goal of transporting 100 tonnes to LEO
Ya I really like their airship to orbit concept. I asked AI about lift to drag (L/D) ratios in plasma at 10,000-17,5000 mph (5-8 km/s) and it suggested that lifting bodies achieve between about a 1:1 and 3:1 L/D ratio. If we assume the generous 3:1 L/D ratio, that would seem to make a single-stage to orbit space plane possible.
A bit off-topic, but an aerospike engine is half of a rocket nozzle, with a virtual half created by the supersonic shockwave. So we could envision a retractable nozzle half that moves through subsonic, transonic and supersonic modes to power the airship.
Also the SABRE engine uses (according to AI) 16,800 thin-walled tubes filled with liquid hydrogen to cool ambient air to -238 F (-150 C or 123 K) in 10 milliseconds so that it can be compressed up to 140 atmospheres and fed into a combined-cycle engine. That would allow it to be air-breathing up to mach 5.4 (3,600 mph or 1.6 km/s) and transition to liquid oxygen after leaving the atmosphere.
I also asked it about using something like titanium to withstand the heat of exiting the atmosphere (since the titanium SR-71 reached mach 3+) but it said that it can't withstand a high enough temperature. So an ablative coating might need to be applied between launches. Quite a bit of research was done for that through about the 1970s before NASA chose the space shuttle with its reusable tiles.
It seems like most of the hard work has already been done to achieve this. So I don't really understand why so many billions of dollars get devoted to other high-risk ventures like SpaceX. When for a comparatively smaller amount of money, a prototype spaceplane could be built. I'm guessing that the risk/reward value just wasn't proven yet. But really shouldn't VC money chase the biggest bet?
This is the kind of stuff that I went down rabbit holes for when I dreamed of winning the internet lottery. Now that AI is here, I can feel the opportunity for that slipping away. A more likely future is the democratization of problem solving, where everyone knows everything, but has little or no money and doesn't want to pay for anything. So really not much different from today. So maybe it's better to let these half-baked ideas go so that someone else can manifest them.
One of the problems with space stations is that we can make them longer, or we can pull off pieces and replace them with bigger ones. We don’t have a way to make them larger around.
And the way contact points work, I don’t think we have a way to even inflate a new section around an existing one.
I just saw a ship that looks like some of those pictures earlier today: The Beckett-Class science vessel in the Cygnus point of interest by the current Elite Dangerous community goal station at HIP 87621.
Love the painting of the huge toroidal space station—with the houses and forests inside.
I had a thought experiment: if you could ride a bicycle (motorcycle?) against the direction of spin of the station you would essentially be "stationary". You would still have a velocity into the always-sloping-up wheel. What if you rode up a gentle ramp? Could you break away from the surface of the wheel then and become "weightless"?
A big potential problem for an inflatable tube in space is the stress on the walls increases linearly with the diameter. I.e. the tensile force on the wall would be (diameter * psi)/2.
This has been suggested before for a permanent station "on" Venus, floating in its atmosphere.
The atmosphere is caustic, but that's just a design material issue. By maintaining a positive pressure, small punctures would just be a loss to O2 supplies; crew wouldn't need any special safety equipment to patch the holes.
Energy could be obtained via solar, chemical engines, or both. Temperature could be controlled by hovering at a spot near the day/night horizon; since the day sid is too hot and the night side too cold, there exists a Goldilocks region.
Venus is generally closer than Mars, with a weak magnetic field that would help reduce radiation (along with the atmosphere).
21 comments
[ 0.18 ms ] story [ 39.2 ms ] threadBuilding a station this large is gonna be costly even within the cargo hold of starship. But six of them, gutted of insides as welded end to end could provide the vast majority of the bulk mass.
This assume rather sophisticated orbital welding and object manipulation; but its feasible we could do it with robots.
Reminds me of a short sci-fi story:
> The engines are part of the orbiter, so they can be brought home and reused. The solid boosters drop off minutes after liftoff and are recovered for refurbishment. Even the unmanned heavy-lift cargo launchers use the same basic system. But until our group came along, the huge external tanks were simply dumped, after fueling the shuttle to almost orbital velocity.
> [...] The main purpose of the design is simply to keep the tanks from falling. The two massive ends of the Farm act like a dipole in the gradient of the Earth's gravitational field, so each deck winds up orbiting edge-forward, like a flat plate skimming. This reduces the drag caused by the upper fringes of the atmosphere, extending our orbital lifetime.
https://www.davidbrin.com/tankfarm.htm
Maybe I'll go ask the AI.
A rigid ring can resist some of this inherently, but a rigid spoke to the hub cleanly takes up all the inward forces.
If your ring is not rigid, any perturbations can cause oscillations that throw the whole thing out of balance. Like a gas leak in one compartment adding thrust at a weird angle. Soon the whole ring will be oscillating along its plane, which is obviously bad. You can actively correct with thrusters on each segment, but that's a lot of extra complexity.
Basically it's all about stability. A big rigid object is much harder to shake apart. A metal circle will stay a circle in a lot more circumstances than a circle of rope will. Doubly so when rotating in zero gravity.
Flexible tethers are mainly good for small scale. Swinging a crew capsule about a big mass (Project Hail Mary, Stardancer) is indeed cheap and easy. With the complication that you must completely spin down to maneuver or dock.
This isn't new. It's the same person who used to say "but Google said...!" This is a solvable education problem, because we've solved it before.
We have entered an age where humanoid robots are beginning to do many tasks that we thought were exclusively in our domain. At our current pace, I expect they will be able to outperform us in most work settings within a decade or two.
As those robots scale up in their capabilities and numbers, we will send up a fleet of them to space to do the work there. They are far more suited for the environment than humans, and the cost savings would be huge.
[1] Caveat Starship has to reach its goal of transporting 100 tonnes to LEO
A bit off-topic, but an aerospike engine is half of a rocket nozzle, with a virtual half created by the supersonic shockwave. So we could envision a retractable nozzle half that moves through subsonic, transonic and supersonic modes to power the airship.
Also the SABRE engine uses (according to AI) 16,800 thin-walled tubes filled with liquid hydrogen to cool ambient air to -238 F (-150 C or 123 K) in 10 milliseconds so that it can be compressed up to 140 atmospheres and fed into a combined-cycle engine. That would allow it to be air-breathing up to mach 5.4 (3,600 mph or 1.6 km/s) and transition to liquid oxygen after leaving the atmosphere.
I also asked it about using something like titanium to withstand the heat of exiting the atmosphere (since the titanium SR-71 reached mach 3+) but it said that it can't withstand a high enough temperature. So an ablative coating might need to be applied between launches. Quite a bit of research was done for that through about the 1970s before NASA chose the space shuttle with its reusable tiles.
It seems like most of the hard work has already been done to achieve this. So I don't really understand why so many billions of dollars get devoted to other high-risk ventures like SpaceX. When for a comparatively smaller amount of money, a prototype spaceplane could be built. I'm guessing that the risk/reward value just wasn't proven yet. But really shouldn't VC money chase the biggest bet?
This is the kind of stuff that I went down rabbit holes for when I dreamed of winning the internet lottery. Now that AI is here, I can feel the opportunity for that slipping away. A more likely future is the democratization of problem solving, where everyone knows everything, but has little or no money and doesn't want to pay for anything. So really not much different from today. So maybe it's better to let these half-baked ideas go so that someone else can manifest them.
And the way contact points work, I don’t think we have a way to even inflate a new section around an existing one.
I had a thought experiment: if you could ride a bicycle (motorcycle?) against the direction of spin of the station you would essentially be "stationary". You would still have a velocity into the always-sloping-up wheel. What if you rode up a gentle ramp? Could you break away from the surface of the wheel then and become "weightless"?
See e.g. https://www.theverge.com/2024/7/25/24206219/nasa-sierra-spac...
The atmosphere is caustic, but that's just a design material issue. By maintaining a positive pressure, small punctures would just be a loss to O2 supplies; crew wouldn't need any special safety equipment to patch the holes.
Energy could be obtained via solar, chemical engines, or both. Temperature could be controlled by hovering at a spot near the day/night horizon; since the day sid is too hot and the night side too cold, there exists a Goldilocks region.
Venus is generally closer than Mars, with a weak magnetic field that would help reduce radiation (along with the atmosphere).