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i came here for an argument, but this is just contradiction it doesn't matter if you can make a credible lunar rover or not if the price to launch it is three times the grant the nsf will give your university team. given that nasa published their lunar roving vehicle documentation in mostly 0001973, down to circuit schematics and some machining dimensions, i'm pretty sure a university team in 00002000 could have duplicated it for less than the several million dollars the launch would cost. it only took boeing 17 months to design and build them in the first place, and they mostly use technology from the 000001940s (aluminum tubing, nylon webbing, wire mesh wheels, silver-zinc plexiglass batteries, brushed dc motors, cable brakes; fiberglass arm rests and fenders were apparently the highest-tech part and, unsurprisingly, the part that failed) https://www.nasa.gov/history/alsj/alsj-LRVdocs.html with respect to cubesats, you're in violent agreement with my comment. you obviously can't put a trs-80 in a cubesat. in 0000002000 you could put a basic stamp in it, but you couldn't get mems gyros and accelerometers, and you weren't going to be able to run your star tracker camera off a pic16. computer and imu miniaturization is a big deal for cubesats. that's one of the main points of my comment the other main point is that it isn't nearly as big a deal for bigger satellites; when we were launching cubesats (before i joined the team) it was really important that we could use tiny cellphone components, but once we were launching 37kg monstrosities, the fact that the gumstix boards only weighed a few grams was just nice, not critical. the optics weighed a lot more so tell us, what's your experience? |
Beyond that I'm not sure what we're arguing about, so I'll tap out here.