My other question would be whether this is due to the need to radiation harden stuff? We were developing for what effectively was equivalent to an arduino in terms of processing power due to the need for radiation hardening (and other legacy / slow moving reasons).
It depends on the spacecraft. DSN is currently talking with the Mars Reconnaissance Orbiter at 1 Mbit/s (https://eyes.nasa.gov/dsn/dsn.html, select MRO, click "more detail" in the bottom-left).
Unless we can convince congress and NASA execs to increase the budget and get more dishes built pronto.
But the problem remains the link from Mars to earth, not from the surface to orbit.
RANGE 20.00 billion km
ROUND-TRIP LIGHT TIME 1.54 days
DATA RATE 160.0 b/sec
Amazing.
It's been a very long time since I read about it so I cannot provide my source but yes that is likely part of it. There's also the resilience of the components to trauma to consider.
Unfortunately big transistors are old transistors. Modern 7 nm geometries are much too small to be rad-hard. Rad-hardness needs big 20-year-old geometries or even older. That also implies slower clock speeds.
I had no idea that we still monitored these things from the ground.
But they probably can't just buy it from industry, it has to be custom made for the project, with some gov-heavy regulation no doubt.
But surely they could do far better than 1 megapixel.
https://space.stackexchange.com/questions/1336/what-thicknes...
^^ Interesting read on this very topic.
The ISS has off-the-shelf notebooks, but apart from that the uptake of regular non-hardened hardware is relatively recent and quite slow. I think the Falcon 9 has a couple non-hardened systems, and of course Ingenuity has lots of regular off-the-shelf hardware. That was one of the big reasons the predicted lifespan of Ingenuity was so low, but software mitigations (like the ability to reboot mid-flight) have proven very effective.
But who are we kidding? A group of internet forum nerds coming up with something that the people at NASA/JPL/ESA/etc haven't already considered?
NASA's funding problems would compound if they took an attitude this naïve during what is largely a PR mission.
What do the people who are paying for the mission expect to see, is the more meaningful question. NASA's PR department could certainly adopt a strategy of telling the taxpaying public why they are wrong to want what they want, and maybe even mix in some whinging about the available bandwidth, but I expect that is not the best strategy when it comes to congressional funding.
This really does suck, since scientific missions will suffer while this is going on. Screwing up the funding opportunity would suck more in the long run.
(there's a happy medium between 24/7 streaming video and the lame stuff you're proposing, I would think. Occasional short videos for a public with the attention span of a gnat? I am sure NASA has people with opinions on this.)
> And you know this
Persuasive!
Maybe even in triplicate for a consensus system!
Also keep in mind this isn't even for the highest class parts, this is more in line for something like a NASA Explorers program level [0]. Something you would get for a JWST or an Artemis level of program would be even more $$$
Radiation hard electronics are not.
And you don't have to send everything high quality. But at least some shiny pictures would be nice.
Such is space. Everything needs to be designed specially for it, especially for trips beyond LEO (where the magnetosphere is still providing you significant protection).
https://spectrum.ieee.org/nasa-designed-perseverance-helicop...
Bigger focal plane means more power, more data processing/storage means more power. More power means more solar arrays/batteries. More solar arrays/batteries means more mass. More mass means larger actuators to move it around. Larger actuators means more power...all of the above means more money.
I can't give a specific reason why, but there are likely cascading effects and system impacts to the mission. Its not like larger space rated focal planes, larger data storage and high powered amplifiers to get more data down don't exist. But at some point you do just have to call it "good enough" or "meets requirements" to avoid the system spiraling out of control.
The bandwidth depends upon the power levels, antenna size, signal strength and the noise level. See the Shannon-Hartley theorem for details.
This means from a small lander on the moon all the way back to earth the bandwidth is small. Sure put a big camera on there, but it'll take weeks to send one picture in its entirety. The Indian lander only has like 2 weeks of life total.
I mean, how would we communicate with Mars colonies when the earth and mars are at opposite sides of the sun without some series of satellites in a elliptical orbit possibly at angle perpendicular to our general orbital planes?
Is this a reason why India's moon craft had such low resolution images? I checked and the rover only has 2x 1 megapixel cameras for some 3d stuff. The pictures from the lander were the usual low res generic stuff we've always gotten.
Why cant they put a 4k lense on these things? That has to have scientific value even for looking at their own rovers/landers for defects.