But luckily it automatically readjust itself to earth automatically every half year exactly for these events. So on 15.10 we will know, if it is really lost. In either case, the end of its mission is near anyway, because the nuclear batteries are near its end.
edit: Nasa has a blog post on this https://blogs.nasa.gov/sunspot/2023/07/28/mission-update-voy...
(1) https://www.theregister.com/Design/page/reg-standards-conver...
It's also near the end of its usable life so it wouldn't be worth it anyway.
And actually, according to https://voyager.jpl.nasa.gov/mission/status/ it's actually 19,936,472,690 km from Earth so I think like 20ish light hours or so.
https://voyager.jpl.nasa.gov/news/details.php?article_id=118
https://www.youtube.com/watch?v=586Zn1ct-QA
https://www.youtube.com/watch?v=vUvzgZt1Vug
There's a part 3 with a tour of the complex.
Earth is approximately 150 million km from the Sun
Sunlight intensity falls off with the square of distance (ignoring any additional small losses from space dust / scattering from gases etc), so twice the distance = a quarter the solar flux. At the Earth it's ~1361 watts per square meter.
Voyager 2 is approximately 133 times further from the Sun than Earth is, which means it receives optimistically 1361 / (133^2) = 0.07694 watts per square meter.
I found a JPL article [1] that says the RTG onboard Voyager produces 40% less power than it did at launch, and the Wikipedia article [2] says it produced 470W at launch, which means it makes ~280W now.
Wikipedia [3] suggests the solar panels available at the time of Voyager's launch in the late 1970s could convert ~10% of incoming solar power to electricity. Modern panels bring that up to 30% but the designers of Voyager did not have access to time travel.
So at present distance Voyager would need approximately 36000 square meters of solar panel to produce the same amount of power.
[1] https://www.jpl.nasa.gov/news/a-new-plan-for-keeping-nasas-o...
[2] https://en.wikipedia.org/wiki/Voyager_2#Power
[3] https://en.wikipedia.org/wiki/Solar_panels_on_spacecraft#His...
https://www.jpl.nasa.gov/news/nasa-mission-update-voyager-2-...
32 billion kilometers is about 100 times the distance a satellite travels from earth to Mars. [1]
That Earth-Mars trip is estimated in the same article to take 4 months, so figure 400 months or 30+ years to shoot another satellite out to reach Voyager 2.
This is ignoring planetary slingshot math, the extra speed to 'catch' voyager 2, and surely lots of other details. Personally I find years and "mars" to be more intuitive in this case than trillions of football fields.
[1]https://mars.nasa.gov/mars2020/timeline/cruise/#:~:text=The%....
The JPL doco (>>36941433 >>36942321 ) calls it "Command Loss".
"... and celestial referencing instruments (Sun sensor/Canopus Star Tracker) to maintain pointing of the high-gain antenna toward Earth"
This is what the Freedom of Information Act is for:
https://www.nasa.gov/centers/armstrong/FOIA/request.html
The report may not exist yet, so you may need to wait.
This has a good breakdown: https://www.reddit.com/r/Asimov/wiki/seriesguide/
edit: Somehow I got Foundation mixed up with Banks' Culture series. I think I have gotten through most of Foundation if not all but I've had a hard time with the Culture series, there I usually start with Player of Games..
[0] https://www.goodreads.com/book/show/35921.On_Basilisk_Statio...
https://en.wikipedia.org/wiki/Voyager_2#Communications
https://en.wikipedia.org/wiki/Parabolic_antenna#Beamwidth
How about this antenna? https://en.wikipedia.org/wiki/Very_Large_Array
Or this one? https://en.wikipedia.org/wiki/Five-hundred-meter_Aperture_Sp...
Normally I'd have marked the entire subthread offtopic, but hutzlibu's comment deserves to be at the top, even if it does use the word "bricked" wrong.
Here is a photo from Voyager 1 at a distance of 4Bn miles:
[1] https://en.wikipedia.org/wiki/International_Cometary_Explore...
https://voyager.jpl.nasa.gov/news/details.php?article_id=129
https://voyager.jpl.nasa.gov/news/details.php?article_id=129
https://skyriddles.wordpress.com/2023/07/03/stereo-a-comes-h...
"- African dung beetles orient to the starry sky to move along straight paths
- The beetles do not orientate to the individual stars, but to the Milky Way"
https://www.cell.com/current-biology/fulltext/S0960-9822(12)...
https://www.science.org/content/article/dung-beetles-navigat...
https://www.nasa.gov/sites/default/files/ivv_grubb_nasa_ivv_...
On the other hand, at one time there was a physical "proof test model" of the Voyagers.
https://www.jpl.nasa.gov/images/pia21734-voyager-test-model-...
https://space.stackexchange.com/questions/43803/how-did-the-...
[0] https://www.baen.com/on-basilisk-station.html
[1] https://www.baen.com/readonline/index/read/sku/0743435710
Voyager 2 is 160.7 AU.
Light falls off in brightness to the distance squared. So the sun will be 160.7^2 = 25824.5 times fainter for Voyager 2 than it is from Earth. (Since Earth is at 1AU)
The apparent magnitude of the sun from Earth is -26.72. Each step in magnitude is multiplying by 2.512. (2.512^5 = 100, so 5 steps of magnitude is a factor of 100).
log2.512(25824.5) = 11.0295.
11.0295 + -26.72 = -15.6905.
The apparent magnitude of the full moon is only −12.74 (lower is brighter). So for Voyager 2 the sun is still several times brighter than we see the moon. The sun is still many many times brighter than the next brightest star in the sky, Sirius, which has an apparent magnitude of −1.46.
Sources: Voyager 2 distance is https://voyager.jpl.nasa.gov/mission/status/ all else is Wikipedia.
No it isn't. It's 20 billion kilometers. It's closer than Voyager 1.
Second order calculations use careful analysis of the signal pattern in telemetry data- IIRC you can see a slow stretch of the phase which can be used to estimate distance and velocity with high accuracy.
Voyager, along with Apollo, stand as the finest examples of human engineering done yet- we got a bunch of people to the moon and back, and built a probe that still operates 50 years later... farther than anything else humans have launched... I'd be lucky if I can deploy my web app once a week.
Imagine deploying a billion dollar piece of hardware and hoping that it has enough intelligence to keep itself from burning up before you can reestablish contact!
Here is the Australian Standard for Caravan and light trailer towing components, Part 1: Towbars and towing brackets
https://store.standards.org.au/product/as-4177-1-2004
There are thousands of these documents covering everything to do with transport from the vehicles to the reflectivity of street signs.
The regulation (at least in my state) is that only engineers who are registered as Registered Engineers are permitted to carry out professional engineering services in this state.
"Software Fault Tree Analysis (SFTA) is a top-down approach to failure analysis which begins with thinking about potential failures or malfunctions (What could go wrong?) and then thinking through all the possible ways that such a failure or malfunction could occur. Fault Tree Analysis (FTA), is often used by the hardware teams to identify potential hazards that might be caused by failures in hardware components or systems, but with the SFTA, the software isn’t considered the hazard, but it can be a cause or contributor when considered in the context of the system."
"The Software Failure Modes and Effects Analysis (SFMEA) is a bottom up approach where each component is examined and all the possible ways it can fail are listed. Each possible failure is traced through the system to see what effect it might have on the system and to determine if it results in a hazardous state. Then the likelihood of the failure and the severity of the system failure can be considered."
But, to the earlier post, these are driven by hard requirements; specifically adherence to NASA STD 7150.2 and NPR 7150.2. Developers/contractors can tailor/waive them with pre-approval but, in general, they tend to go in the direction of less requirements, not more. This may all be moot because I think Voyager pre-dates any of those requirement documents and I'm not sure what existed in the late 1970s.
Supposedly you could literally slap them out of the air if you were at the muzzle, when they had just begun accelerating.
They were in the James Bond movie You Only Live Twice.