Found my starting point. The registers can be built with a bunch of these D-type 3 state flip flops:
74ALVCH16821
PDF Datasheet https://assets.nexperia.com/documents/data-sheet/74ALVCH16821.pdf
According to my rough calculations, I need an O'Neil Cylinder built in Earth's Larange point 5, with a diameter no less than 1.14km and length no less than 7.61km, to support a renewable forest for firewood for a single a wood stove in a single orbit
Seasons like winter can be simulated with solar shading and moisture pumped through a central line of needle spray nozzles. The Coriolis effect on falling snow and rain would be remarkable
Maintaining this wouldn't require much processing power
TIL This is the "noise" captured by Voyager 1 in the interstellar medium. I can't be entirely sure there are no space whales
Wonder how practical it would be to build something approaching the Voyager probes' durability in my living room
http://www-pw.physics.uiowa.edu/voyager/v1pws_interstellar_epo.html
A DIY space program needs lots of antennas
It's possible to build a fairly adequate parabolic dish (beam waveguide type so the base is stationary) with EMT electrical conduit. The dish just needs to support itself and EMT conduit is fairly easy to bend to the correct shape and is robust enough to survive outdoors even under heavy snow
There's a lot of "X has more processing power than the Apollo lander" and similar phrasing and that's usually not a good comparison
Spacecraft hardware is highly specialized and extremely capable in the narrow field in which they're used
From a biological perspective, it would be like comparing brain size and neuron count. Behavior is a lot more accurate indicator of intelligence and capability
I can't even guess how smart an octopus is, but we don't typically use their size to compare
And speaking of space hardware, being resilient is often more important than just capability and speed
In fact, most space-rated hardware is going to be slower than their consumer counterparts, but that's OK because the software is highly optimized to run on it
The trick to getting the DIY space program operational on that front is making sure the hardware is resilient and the programming optimized and actually fits the purpose more than increasing raw speed
This is by far one of the better animations of a rocker bogie that I've seen in a good while. It moves the middle suspension bar to the rear, which frees up the middle for actual storage, power etc...
This is by far the simplest practical breakdown of the rocker bogie mechanism that's easy to understand. It's one thing to read papers with angle calculations, pressure delta etc... but another to actually see just the moving components
I think this platform would work quite nicely for the simplest practical rover
https://wpirover.wordpress.com/2011/11/15/rocker-differencing-kinematic-suspension/
And then there's this guy who built an entire rocker bogie car for his kid
There's a lot of reading involved when it comes to starting your own space program
Personal hygiene is important under the DIY space program. Of course, a spinning habitat would make things a lot simpler, but in the meantime, we'll probably go with the no-rinse shampoo too
https://www.reddit.com/r/Damnthatsinteresting/comments/jp76rj/washing_hairs_in_space/
I was looking at the engine detail of the Redstone rocket engine, the heart of the PGM-11 missile. It occurs to me that this particular geometry lends itself quite well to the expander cycle
This particular engine had a turbopump powered by decomposed high-test peroxide
In theory, H2O2 is a pretty neat way to power a turbopump (also used by Copenhagen Suborbitals is using it for their engines) and as a monopropellant for RCS thrusters, but it's kind of a pain to handle and store safely
Fiber optic cables don't seem to fare well without special shielding and different methods of construction in a high radiation environment. While they're resistant to transient EM spikes, they do tend to break down and attenuate more of the laser light over longer distances
This is a bit of a dilemma. Either go with copper lines for signaling and sensors and risk spikes and have them acting as antennas in a EM field, or go with fiber. Alternatively, I may have to make my own
Speaking of explosions...
The number of accidents in rocketry is too damn high!
Some of that is the inherent danger of the fuel + oxidizer and the complicated plumbing involved. I have neither the intelligence or patience to grasp all of that mess so if I build a rocket, it will probably use the expander cycle
The plumbing is *far* less complex with fewer moving parts. Which means fewer places for things to go wrong and fewer areas of concern to monitor (less work for the computer)
I know the new hotness is Methane right now, but I'd go with Dimethyl Ether as the fuel instead. It's very cheap and can be made from biofuel (possibly on Mars via a different process as well)
As the oxidizer, I'd use Nitrous Oxide. Laughing gas, basically. It's also very cheap and made by the millions of tons. Best of all, it can be decomposed into a very hot gas at 577 C
Dimethyl Ether auto ignites at only 350 C so there's the startup process solved. No need for pyros, sparks, etc...
No nonsense that can fail explosively. Just a tiny electric pump to get the N2O going over the catalyst, which is more than hot enough to ignite the mixture
Also, the expander cycle limits the maximum size of an engine, which means you have to build more smaller ones anyway. While that's extra work, you get spares if one or two shutdown mid-flight
And expanders don't have complicated turbopumps which need high temp/high speed moving parts and seals so they're cheaper to build
Going with Dimethyl Ether and Nitrous Oxide as fuel and oxidizer also because they can be kept liquid at similar temps
-141 C To −24 C for Dimethyl Ether and −90.86 C to −88.48 C for Nitrous Oxide. Which means, they can share a bulkhead in the tanks
This significantly cuts complexity and reduces weight
Also, both have enough expansion at warmer temperatures that I can use "Autogenous pressurization". Same as SpaceX's Starship (though mine will probably be made of glue and aluminum foil)
Apparently a turbocharger from a V8 isn't actually designed to funnel liquid propellant at -89 C at turbopump tolerance. Or survive reentry down from orbital speeds (because reusable rockets or GTFO)
My plan to use a rice cooker to make homemade high-temp composites is probably gonna have issues too
I hope lockdowns lift a bit so I can go trash diving. I'm sure someone's thrown out an orbital grade turbopump somewhere
Although there are significant drawbacks with a multi-nozzle rocket engine design, I think for small scale development, the benefits outweigh them. Biggest benefit being combustion stability, which is greater in smaller combustion chambers (see Apollo's F1 issues). The biggest drawback is the additional manufacturer of nozzles and chambers, but once you get the design finalized, they're relatively straightforward to do repeatedly
So far, I've been unsuccessful in finding an appropriate spacesuit design that I can make with my own sewing machine and materials from the craft store. Probably will have to settle for a pressure suit made of heat resistant material for now, until I get better at it
I'd like to investigate non-pressurized suits, particularly compression types which use "lines of non-extension". The materials will still be expensive, but at least this will be old research
Today in gloriously-impractical-yet-want, here's an actual core memory unit including the Gerber files for the circuit board and schematic
http://mikesmods.com/mm-wp/?p=556
Spacecraft don't use these anymore since there are better options, but part of me feels like there's still some value in here
I also wonder if it's feasible to have core memory backed SRAM
So the system reads/writes to SRAM in normal use, as a fast buffer, while it slowly updates the core memory
Might just be crazy enough to work
@th OK, this right here is the reason the Internet is awesome