Launch loop
en.wikipedia.org
en.wikipedia.org
https://www.youtube.com/playlist?list=PLIIOUpOge0LsGJI_vni4x...
The thing I love about Isaac Arthur is that he does these collaborations in part to drive some of his traffic to smaller channels that are just as interesting. He's a fantastic guy.
[1] https://www.youtube.com/channel/UCEszlI8-W79IsU8LSAiRbDg/vid...
The amount of fuel required to circumnavigate around the world on a jetliner is on the same order of magnitude of going into orbit. The spacecraft has to carry about three times as much fuel when loaded than the jetliner does (it can stop three times.) The vehicle is more expensive than a jetliner but not impossible so, the ticket price could drop to 3x to 10x what it costs to fly around the world.
The main advantage that the airliner has is that they can get you out of the airliner, check and clean the plane up in 30 minutes to an hour, fuel up, and be flying another bunch of passengers to the next destination.
If you are using throwaway vehicles you can't approach the cost of air travel. You can't do that with a Space Shuttle that takes 6 months for technicians to check out every single thermal tile.
Speculative concepts such as space elevators and scramjets don't compete against the Space Shuttle and the Saturn V, they compete against highly evolved versions of current technology, which can achieve huge cost reductions by accelerating reusability.
It would be nice to get to orbit without sitting on top of a marginally controlled bomb.
Then you would hate a launch loop. A flexible steel rod traveling at above orbital velocity and magnetically suspended inches away from an enclosing sheath is basically 200 miles of kiloton explosions waiting to happen, followed by an unimaginably large rain of debris.
Still, you only need to perturb your orbital plane a very tiny bit to be out of the way of future launches, and then you have all the time in the world to navigate to where you want to go.
Also how many different inclinations are actually required to serve 90-95% of all launches? There's really only a handful of inclination 'classes' out there that would need to be fulfilled; 0 for geostationary, 51.6 for ISS (assuming it's still up when we build the loop), 80-90 for various Earth observation and communication satellites. If we can super cheaply launch satellites into a couple defined inclinations most customers would probably be able to make do with one of these common inclinations rather than today where they'd go with the perfect one.
Rockets conveniently spread the impulse out over a long period of time.
The launch loop changes everything, because your launch costs are in the neighborhood of $3 per kg. That's a total shift in the way we think about rocketry.
Imagine if gasoline was $4000 a gallon. In that world, driving 20 miles to the store to pick up some groceries would be unthinkable.
In conclusion: if you liked the launch loop idea but haven’t read Seveneves then go buy/download it right now!
Could you drill a tunnel that's basically a chord (line between two points on a circle) that runs through the Earth between two surface locations, put a fully evacuated Hyperloop type system into it, and fire objects into space with maglev acceleration? It would be a full vacuum until the object neared the exit end at which point it would open. Air would rush in of course, but the object would need a heat shield anyway and would have to be traveling many times faster than escape velocity.
I guess it's a variation on gun launch.
A 20-minute video explaining the concept: https://www.youtube.com/watch?v=J1MAg0UAAHg
I think many times we start with the ideal: what if we just had a cable reaching into space that allowed us to easily get up there?
And then from there, they work backwards on how that would be engineered.
Or was it, he had some fascination with rotors and thought of a really big version of some similar, smaller version he had thought of before.
idk
When your system is one giant 62,000mT cable with the kinetic energy of 62 Hiroshima bombs, I think you'll lose your $30B investment pretty quickly.
I may not know too much about spaceflight, but I do know that gravity tends to pull downward, towards the earth. I don't see cables doing a good job of suspending these things in the air when they are constructed beneath the structures...
The "support" comes from the momentum of the moving parts within the cable.
Apparently traditional skyscraper building techniques could be used to build a single structure 11 miles tall. Again, no one would do it, because it's not economically justifiable. Maybe if there was a space tower cold war?
it might have to be at the poles.
another option would be to build a bridge from south america to west africa, and at 1g you'd reach escape velocity.
A Tesla Model S can accelerate at 1.14g while going from 0-60mph, but it can't continue that acceleration for long.
A dragster can accelerate at 5g for almost a second. It won't get into orbit if you send it off a ramp.
The train with a centripetal acceleration of 2g will not launch anything into orbit unless it can magically keep providing that acceleration to the vehicle.
On the other side, you don't need to accelerate particularly hard if you want escape velocity, you just need to get up to that speed after accounting for atmospheric drag. You could launch a winged rocket that accelerates at 1.12meters/s^2 -- in ten thousand seconds or so, it would be up to escape velocity.
But Fortaleza, Brazil, to Dakar, Senegal, is about 3100 km. 1G over that distance gets you to 7795 m/s, after 795 s. That can almost get you to a LEO, with a 40 degree inclination. You'd still need to overcome atmospheric drag.
Fortaleza, Brazil, to Libreville, Gabon, is 5350 km. 1G over that distance gets you to 11240 m/s, after 1045 s. That will get you into an orbit with 4 degree inclination, and after accounting for drag and the angular velocity at the equator, you might even still be at escape velocity after exiting the atmosphere.
That means it already has higher angular velocity by virtue of being close to the equator, and is further from the Earth's center of gravity by virtue of being situated on the equatorial bulge. The peak is also 45% the atmospheric pressure at sea level.
The floating tunnel would be about 1100 km, and then about 150 km up the volcano. At a constant acceleration of 30 m/s^2, relative to the launch tube, 1250 km of track gets you up to 8660 m/s after 289 s. Then you get 464 m/s from changing reference frames from Earth-fixed to Earth-relative at the peak of the volcano. Subtract about 1300 m/s for drag, and 7824 m/s is roughly a LEO at 200 km. About 3 Gs for about 5 minutes is easily tolerated by healthy humans in the correct orientation--we do that in amusement park rides for fun.