The concern is that the second stage didn’t perform as expected. What if that affects the primary mission on the next flight? They need to understand the root cause before they fly again.
As the article states, the upcoming Europa Clipper launch requires an upper stage relight to put the spacecraft on the desired trajectory. If the second burn does not go as expected, the mission could be in jeopardy.
The router on this page uses a switching regulator. Switching regulators have a relatively constant power draw over the entire input voltage range.
But just because you know the protocol dues not mean you have enough information to send a valid command. The commands are wrapped in a common protocol, but the commands themselves are typically mission-specific and definitely not made public.
Here’s an example of someone unaffiliated with the mission decoding JWST telemetry. While they were able to identify the packets defined per CCSDS protocols, they do not know the actual content of the packets, which are mission specific.
https://destevez.net/2021/12/decoding-james-webb-space-teles...
And as someone else mentioned, the biggest hurdle with getting a command to voyager is access to a 70 m dish. Not many of those floating around…
It did, so slow clap for the engineers for saving a very expensive science experiment remotely from billions of miles away. well done.
I think the unstated is that the original group of scientists feels like they are being put out to pasture in favor of a new set of researchers. But as you mentioned, if there aren't any more Kuiper belt objects on the "horizon", it seems like the right move.
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Does this mean it has only a 12-hour window to transmit? Or there's multiple antennas on Earth?
However, the ground stations are shared between many missions, so they are not available for JWST all the time. Expectation is that JWST gets 8-12 hours/day of DSN time.
Hope the SSD does not fail after 32768 or 40000 hours of operation.
JWST does not use a typical flash-based SSD. The mass storage is all SDRAM. There are layers of error correction and scrubbing to handle bit flips.
0.028*3600 = 100 Gbit/hour
No problem here.
Everything was sized based on the expected volume of data that the telescope would be able to take. The instruments only generatedata at a certain rate, and there are inefficiencies involved with slewing between targets. Having a larger recorder or faster downlink would not mean that JWST could take more science data.