Space Tethers: Stringing Up the Solar System
toughsf.blogspot.com
toughsf.blogspot.com
But it seems like you have to trade power for accuracy; if you can hit a tiny window moving in three dimensions inside of a 3 body problem, then you don’t need to be able to manage as much delta V (increasing to leave, or decreasing to land). Smaller rockets, less need for ablative materials.
But if you miss, boy are you fucked.
One solution for this I’ve heard is you take enough fuel to get where you’re going with plenty to spare. If everything goes right, you offload your emergency supplies (reaction mass, fuel) and get a credit.
I’m not sure how much handwaving goes along with moving liquids and gasses in vacuum, at zero g... burst a line you need a lot of reaction mass to reorient yourself.
Maybe there’s an emergency venting design where all of the forces cancel out...
Imagine closing in on Mars knowing that if you fuck up a super-orbital speed, split second maneuver by more than a couple of meters you will drift in space until asphyxiated. It makes a carrier landing seem bland.
If you carry enough fuel to decelerate without the tether it defeats the purpose of the tether.
And it might be easier to store the emergency retrieval system on the tether's hub. That way it doesn't have to be hauled around to be used (hopefully) infrequently.
Maybe there could be uses for the fuel, if you succeed in getting it there.
You are coming in at hyperbolic velocity and have to use the thin and very variable atmosphere to break into an orbit.
At least the tether is completely predictable.
If it works in KSP, it will probably work in reality.
I think the idea is brilliant, since you don't need rocket fuel to to generate the force you would transfer to the craft.
But with the bridge, it’s just distance you’re crossing. With a tether you’re also dealing with velocity. And changing velocity changes distance...
Then what is the point? 90+% of spacelaunch is lifting fuel, and the fuel you need to lift that fuel, and and and... all fuel. The whole thing is an exercise in moving reaction mass around using other reaction mass. Hauling around an extra 2km/s of deltaV would require a rocket on the pad double or triple the size of not bringing it. Spacelaunch equipment has to work every time or else it isn't worth the investment.
Even if we treat the tether as a potential 'bonus' rather than a necessity, think of all the fuel spent on the intercept with the tether. Your launch time would have to coincide with the tether, meaning you launch at a non-ideal time. And you would only every launch into the tether's orbital inclination/plane, radically reducing the number of potential destinations.
You could imagine one company having a more reliable but expensive launch platform and another having a cheaper one that occasionally explodes, or has a smaller launch window. You'd fly up fuel on the cheap ones, and your deep space probe on the other. And any fuel left from previous missions can be resold or spent on good will.
Essentially instead of 3 stages to high orbit, or 4 stages to another planet, you have 7 smaller stages (2 + 2 + 3) to another planet.
Electric thrusters are getting huge specific impulse improvements and the future seems to be pretty bright for them. We can trade time for efficiency essentially.
For interplanetary transit, just keep the platform running a circuit between the planet and earth. It's going to be way easier to hit your entry without getting into an unrecoverable situation.
http://hopsblog-hop.blogspot.com
Best read in chronological order.
KSP is one of my favorite, infuriating things to exist, and I'm not sure why.
It also seems like there is a conservation of energy issue here that I don't understand. In a state of balanced departures and returns, the energy used to launch departing vessels would be captured from returning vessels, but in the Earth-Mars loop, the returning vessels were themselves launched from the surface of Mars and accelerated by tethers there. It feels like a perpetual motion machine.
RE balance of incoming/outgoing boosts, that's why the article mentions the option of having the ship carry some extra fuel as payload to refuel the tether - because even with that, tethers still get you energetically and economically ahead over having the rocket fly itself all the way to destination, due to exponential nature of the rocket equation.
“ And of course, none of these deltaV savings are for ‘free’. Accelerating payloads means the tether will slow down. If it slows down too much, it will de-orbit itself. The momentum lost with each catch-and-release operation must be recovered either by absorbing momentum from payloads being slowed down, or by using its own propulsion system.
A major advantage of an orbital tether is that you do not have to immediately recover that momentum - it gives time for slower but more efficient propulsion systems like a solar-electric thruster to gradually accelerate the tether. A chemical propulsion system limited to 450s of Isp is not needed as the acceleration can be done over time with something that has thousands of seconds of Isp. The propellant needed to run the tether’s engines is greatly reduced. Even more interesting is the possibility of propellantless propulsion, such as electrodynamic tethers that push off the magnetic fields around a planet.”
Rockets have to balance their specific impulse (efficiency) against their need for massive amounts of thrust immediately. You can't take off from the ground using an ion thruster, despite what Kerbal Space Program tells us.
But a tether system in orbit could be using a very efficient engine to gain momentum over a very long period of time (months, years, etc). Give it large solar arrays or a small nuclear plant on-board. It's getting a much better exchange rate on that delta-V than the rocket, which needs to fight earth's gravity and air resistance.
There are 7 million seconds in three months. That's a lot of time for a Hall Effect thruster running off of solar power at 1 AU to boost the momentum of a tether.
That's not ironic at all!!
But hardly anyone cares.
But several orders of magnitude harder, maybe impossible, it's exciting?
If we can't tether in our atmosphere what chance is there in space.
[1] https://spectrum.ieee.org/energywise/energy/renewables/exclu...
That said, it might be easier in space because there's less atmosphere to worry about (not nothing though, debris and micrometeoroids would probably pose a problem in the long run)
The nobody cares bit is around HN not caring all their info was made open source (Try algolia). There's no reason you couldn't try and pivot. It's something you can contribute code to. Tethers can also supply electricity upwards. You could make permanent platforms, perhaps.
Space tethers are probably impossible, certainly nothing can be started for decades. It's fun to LARP but it'd also be nice to get equally keen about things that are possible and actionable.
> Let’s imagine a modestly-sized tether orbiting at a high altitude above the Earth. It is 1,000 km long...
The video in the article is here: [1] and the sources to the video [2].
The usual way they talk about keeping these things aloft is to set up an electromagnetic accelerator track on the moon and aim buckets of ore, or industrial product, at the upper rim. They latch on at the top and get dropped off the bottom.
Timing is critical. It takes computers.
All around the circumference you have radial tethers with scoops at the end. You just have to dive into the scoop when it dips down in front of you. Then it's a wild ride up and out.
Power production (or thrust if reversing the process by feeding a current into the wire) is described in [0].
Use for stabilization and attitude control is described in [1]. These might be combined with [2], which have more immediate effect but from time to time need to be 'desaturated' which is where [1] comes in again.
[0] https://pwg.gsfc.nasa.gov/Education/wtether.html
[1] https://en.wikipedia.org/wiki/Magnetorquer
[2] https://en.wikipedia.org/wiki/Reaction_wheel#Implementation
You cannot really "hold" something in place (barring an external propulsion system that costs energy), so while you could extract some energy at first due to inertia, you will slow the orbiter down and barely collect more (if any) than you needed to put it there in the first place.
An alternative but close system was described in Stephen Baxter's Sapce (Manifold series), with (IIRC) superconducting loops around Io, to collect energy from Jupiter's magnetic field, technically extracting energy from Io's momentum.
By the time we can build these we should be up to our eyeballs in fusion energy. Seems like you could just build giant 50km railguns to blast raw materials and a kick stage into orbit and leave rockets for the squishy payloads.
It probably doesn't take anything special like a 50km railgun. We probably could have one by now if we had of just not stopped Gerald Bull's Canadian funding rather than assassinating him.
https://www.imdb.com/title/tt0109650/ https://www.youtube.com/watch?v=UvL9qcJKqOw
There are a lot of alternatives being worked on, with venture money, that might yield before I die. But the Tokamaks have always been a jobs program to maintain a good population of high-neutron-flux techs ready to draw upon for weapons programs. It is why p-B fusion has never attracted any gov money: no neutrons.