Starliner crew reports hearing "sonar like noises"
arstechnica.com
arstechnica.com
But the fact that this sound is coming through the speaker, and the way it restarts around 1:10 (unless that's just a comms hiccup), makes this seem like some kind of electronics issue. Sounds a bit like an alarm/warning, even.
[0]: https://usa.chinadaily.com.cn/china/2016-12/02/content_27545...
My bet is that the new wiring wasn’t properly RF shielded.
Yet
That is a far more complicated job than sending a manned crew to space, which is, as other have indicated, table stakes at this point. Coming down safely and going back up with the same hardware is the required part of Starliner that massively failed.
Watch the crew entering ISS. Williams is very, very, very happy to have survived the ascent. <https://www.youtube.com/watch?v=zsURePrNTx0>
The last two decades of progress has come almost exclusively from “new space”.
Not for lack of trying
> NASA issued the following explanation on Monday for the strange noises: "A pulsing sound from a speaker in Boeing’s Starliner spacecraft heard by NASA astronaut Butch Wilmore aboard the International Space Station has stopped. The feedback from the speaker was the result of an audio configuration between the space station and Starliner. The space station audio system is complex, allowing multiple spacecraft and modules to be interconnected, and it is common to experience noise and feedback."
https://www.youtube.com/watch?v=PIKDRS5K2uo
https://news.ycombinator.com/item?id=32958319
has this been solved?
(Wooden hammer on a steel bucket!)
Them astronauts have nerves of steel.
Think about the fullness of the waveform to make a sonar ping like that (like in a synth or something). Really weird!
If you don't understand it just watch the movie and listen to the signal picked up from the region around the star Vega, then you will understand.
Edit: I somehow wrote SpaceX even though I knew Starliner is made by Boeing. The news related to X being blocked in Brazil confused me probably…
"Ground" is an arbitrarily-chosen voltage convention. In space the floating ground won't cause a fault because there's never an electrical circuit with both the floating ground and the 'real' ground.
EDIT: turns out the ISS is a bit more complicated than that, and it also has a "grounding strap" that connects to the local plasma. https://news.ycombinator.com/item?id=41417136
Fun tidbit, old English cars (and the original Ford Model A!) used to tie positive DC to the frame rail as a “ground” or “common” instead of the negative DC. They are referred to as positive ground cars (and tractors!)
https://www.restore-an-old-car.com/positive-ground-cars.html
Busses also (used to?) have ground straps that you may see dragging. Apparently this was somewhat common on cars as well. "bus ground strap" is unsurprisingly difficult to search for, but I did find a discussion on Quora [1] that claims rubber formulations were responsible for vehicles picking up a static charge.
All of this is interesting once seen as an attempt to remove the potential difference between local "ground" and ambient environment.
[0] https://en.wikipedia.org/wiki/Static_wick
[1] https://www.quora.com/Cars-used-to-have-grounding-straps-han...
https://s3vi.ndc.nasa.gov/ssri-kb/static/resources/NASA-HDBK...
Apparently you attach all grounds to some common component, like the chassis and then you have a zero volt reference. As long as it is stable and the relative voltages to it are consistent, that should suffice for electrical systems. Handling overall charge of the craft might be a bigger challenge, but no idea how that would be handled.
I guess they use the same solution than during EVA which is running the Plasma Contactor Units to dissipate any buildup.
From the Commercial Crew requirements document[2]:
3.9.3.13 Integrated Space Vehicle Electrostatic Charge Control
3.9.3.13.1 LEO Charging Design Standard
The spacecraft shall meet the intent of the requirements contained in NASA-STD-4005, Low
Earth Orbit Spacecraft Charging Design Standard. [R.CTS.285]
How the contractors achieve that might be proprietary. It looks like (at one time) SpaceX used electrically conductive paint[3] as part of their mitigations.[1] https://standards.nasa.gov/standard/NASA/NASA-STD-4005
[2] https://ntrs.nasa.gov/api/citations/20150010757/downloads/20...
[3] https://phys.org/news/2013-03-white-coating-spacex-dragon-tr...
You will see that it says: "IDSS compliant mechanisms protect against electrostatic discharge through the soft capture system" which is to say not much.
That’s still more than the previous standard for which the paragraph on ESD just says "RESERVED".
[0] https://ntrs.nasa.gov/api/citations/20170001546/downloads/20...
https://ntrs.nasa.gov/api/citations/20110014828/downloads/20...
TL;DR they dissipate charge using three Plasma Contactor Units (PCUs) on the Z1 truss, and measure it using the Floating Potential Measurement Unit (FPMU) on the S1 truss. This clamps the ISS to within 20 volts of the local plasma.
https://en.wikipedia.org/wiki/Plasma_contactor
https://web.archive.org/web/20060929171819/http://space-powe...
https://www.nasa.gov/image-article/floating-potential-measur...
I would assume everything on ISS and capsules are running DC. Does DC need a ground? Every electronic circuit I've built just uses ground as the common leg to battery or power.
Any RF or EMC engineer will tell you that ground is a dirty word, especially in extreme conditions. There's no one-size-fits-all approach, since so much depends on the physical context.
[1] https://radhome.gsfc.nasa.gov/radhome/tid.htm
[2] https://www.analog.com/en/signals/thought-leadership/challen...
SpaceX has nothing to do with it