Nasa proves its space helicopter can fly on Mars
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I realise it's just a concept test for future missions, but this doesn't seem like a particularly rigorous test. I assume they are they under a lot of time pressure.
The difference is more like that this is the first untethered, full-flight-system, full-environment test. The data from which is compared to the huge batch previous tests with partial systems, w/ and w/o gravity offloads, etc etc.
Logging a lot of flight time with the actual hardware is a really bad idea, sort of like "testing in production."
That's a fascinating fact. A lot of work must have gone into a testing environment that can do so much of the work via simulation.
We test in staging environments set to mimic production 100% (or as close as possible) all the time.
After an initial period where they're under development, un-maned aerial vehicles should obviously be tested a hell of a lot in actual end environment, with their whole actual hardware, too.
It worked for Boeing.
But what about power? How long can a 4lb drone fly? a few minutes?
Presumably there's a way to recharge this thing, but that would require a base-station with solar or nuclear power source. I am not understanding how this drone would be effective in a mission!
It's hard for me to imagine a drone not being effective!
https://mars.nasa.gov/msl/mission/whereistherovernow/?ImageI...
For power in particular, charged by solar panels (the things above the rotor), worst case end-of-life flight time is estimated at 90s, depending on season it might take more than 1 day to reach full charge.
Edit: And the two numbers for range I can find in that document suggest 300m flight range, and "outbound sorties" of length 100m (suggesting always flying back to the rover?).
[0] https://rotorcraft.arc.nasa.gov/Publications/files/Balaram_A...
I imagine based on past missions, probably after all objectives are achieved and time on the array is available, they’ll get creative and push the chopper a little more.
Earth gravity is 9.81 m/s^2, mars gravity is 3.72 m/s^2. To emulate this on earth you would have to be on a aircraft accelerating downwards at 6.09 m/s^2. Doing so starting at 0 vertical velocity for 90 seconds would mean loosing 24664.5 meters of altitude, ending at 548.1 m/s. The speed of sound is 340 m/s - so the only reasonable flight profiles (i.e. subsonic) probably involves starting out with ~274m/s vertical velocity, and doing a parabola where you get back to your starting point.
I'm not sure if you could actually maintain the necessary acceleration, and I imagine it would be difficult to maintain an atmosphere simultaneously, but it might be doable.
We have a very good track record of sending large rovers with solar and nuclear power sources to mars. A rover would make a good mobile base station, with a helicopter for collecting samples from various places to bring to the rover's onboard lab.
Well. As I have a strong hosts file as well as respective browser addons I do not care - their trackers do not see me.
There are plenty of good sites out there who have either less or no tracking bollocks, I don't need to use the shitty ones.
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Not going to do that!
And from the Google cache link:
> 404. That’s an error.
> The requested URL /search?q=cache:lT5Qm1nXpPcJ:https://www.engadget.com/2019/03/29/nasa-proves-its-space-he... was not found on this server. That’s all we know.
But the Internet Archive has a good copy: https://web.archive.org/web/20190329140048/https://www.engad...
This sounds like something that could make the helicopter more stable. Could a physicist please explain why it's still a good test?
They could also test the stability by trying to maintain a constant force on the tether (by not simply pulling as hard as possible), but I imagine they have different ways to test stability.
As for the helicopter, ARGOS had to adapt its weight relative to Earth by pulling it up enough to simulate lighter conditions on Mars.