Toray carbon fiber to carry SpaceX's Mars ambitions
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https://m.reddit.com/r/spacex/comments/4y0z6e/toray_carbon_f...
We're decades off. You're asking about the state of supersonic air travel while researchers are still figuring out how to smelt aluminum.
Then even when the cable strength and length issues are satisfactorily resolved, there are lots of other logistics to deal with.
I think any future barriers to the elevator(s) will be more regulatory than technological in the future.
From the perspective of a hypothetical future in which all the technological problems have been solved, the barriers might be regulatory. But that seems tautological.
If an elevator could provide more 9s of reliability, that could be huge.
And when we're talking about human spaceflight, consider the work SpaceX and Blue are putting into in-flight abort and propulsive landing - SpaceX's Crew Dragon should be much safer than the Space Shuttle, for example.
Propulsive landing helps for some failure modes but not all. Like I don't think it would have helped the CRS-7 failure had that been manned.
https://www.nasaspaceflight.com/2015/07/saving-spaceship-dra...
Once we have a rocket-powered transport network between, say, Earth-orbiting space stations, a moon colony, some near-Earth asteroid mines, fuel depots at lagrange points, a Phobos outpost and robotic factories on Mars, the economic payoff of a space elevator will be more immediate. Plus we could try them out on less massive bodies first, like the moon.
However orbital vertical tethers are doable with Zylon. A series of 3 orbital tethers could move stuff between LEO and the lunar neighborhood. http://hopsblog-hop.blogspot.com/2016/08/tran-cislunar-railr...
Both Musk and Bezos seem well on their way to reusable boosters. But reusable upper stages is another story.
An upper stage re-enters at around 8 km/s. An ~7 km/s delta V budget plus the need to carry a payload means a very slim dry mass fraction, an egg shell space craft.
Recovering and reusing upper stages will be much harder than reusing boosters.
The space elevator is an idea that sounds cool but is fucking dumb if you think about it for more than ten minutes, like the idea of accelerating ships to near light speed, when every hydrogen atom in the void will shred your hull like a cosmic ray.
Which part of this is current tech?
Hopefully Congress takes notice within the next few years, and funnels the money currently spent on the SLS rocket to Musk's Mars project.
The bottleneck is not Falcon 9 production, at this point it's largely on the payload side. A faster turnaround would certainly help, but there's only so much optimization that can be done.
The Falcon Heavy is not a priority because (1) much less demand from customers and (2) it's a transitional system between Falcon 9 and built-for-reuse BFR/MCT, so it will have limited use.
I do wish that Falcon Heavy would finally launch though.
"Dilution is the solution" was an unfortunate attitude on Earth. It will work for millions of years in space, and hydrocarbons are pretty abundant.
In recycling the fibers get shorter..
Could not that be re-applied to a different industry as far as re-using the carbon fiber? Body Armour for soldiers as the shorter fibers would be of use there?
The carbon fiber is then chopped and used as reinforcement in other material likes plastics. SGL Group, who supplies/partners in production with BMW, even uses reclaimed and production waste in it's production process for the new 7-series.
A more technical breakdown and state of the industry can be found here: http://www.compositesworld.com/articles/recycled-carbon-fibe...
If you're building a space ship you have very tight tolerances and specifics needed for the alloying of the metals you use. The aluminum in aircraft is full of strange things that need to be removed for general use aluminum and definitely need to be removed for building new aircraft.
You're right that melting and re-casting aluminum is really cheap and efficient for beer cans, it's not so much the same for aerospace aluminum.
When it comes down to spaceships, the energy used to produce them is usually a very small portion of the total cost of the mission and we don't make very many of them – recycling isn't and shouldn't be a priority.
The Falcon 9 burns 110,000 liters of kerosene every launch, if it were made of carbon fiber, maybe it wouldn't matter how the structure was disposed.
[0] Aircraft grade aluminum alloy's composition roughly includes 5.6–6.1% zinc, 2.1–2.5% magnesium, 1.2–1.6% copper, and less than a half percent of silicon, iron, manganese, titanium, chromium, and other metals.
[1] Aluminum cans are typically 1% magnesium, 1% manganese, 0.4% iron, 0.2% silicon, and 0.15% copper.
There are a lot of metrics that determine the appropriate use of various grades of aircraft level alloys [2]. I guess from the outside some big considerations are how the metal reacts to temperature change and how well a metal cylinder can handle stress while staying light.
[0] https://en.wikipedia.org/wiki/7075_aluminium_alloy [1] http://www.madehow.com/Volume-2/Aluminum-Beverage-Can.html [2] https://en.wikipedia.org/wiki/Aluminium_alloy
Are we talking beer cans or rockets? Maybe they are the same after all :)
All spot on. There are lots of alloys used for lots of different things and economics and availability play their part too. When you're designing your airplane every slight detail matters.