A 12-year sequence of telescope images of a star and four planets orbiting
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A 12-year sequence of telescope images of a star and four planets orbiting
Unofficial Hacker News client; not affiliated with Y Combinator.
ortusdux · · focus · HN ↗
<a href="https://www.jpl.nasa.gov/missions/the-roman-coronagraph-instrument/" rel="nofollow">https://www.jpl.nasa.gov/missions/the-roman-coronagraph-inst...
The Roman Coronagraph is designed to detect planets 100 million times fainter than their stars, which is 100 to 1,000 times better than existing space-based coronagraphs. The Roman Coronagraph will be capable of directly imaging reflected starlight from a planet akin to Jupiter in size, temperature, and distance from its parent star.
izend · · focus · HN ↗
lukeify · · focus · HN ↗
As long as the telescope can fit through the Starlink Pez dispenser.
walrus01 · · focus · HN ↗
Such an architecture might not be an impossible design consideration if the goal is to have something big like the sun-shade/cold side of the Webb telescope.
dylan604 · · focus · HN ↗
walrus01 · · focus · HN ↗
NitpickLawyer · · focus · HN ↗
topspin · · focus · HN ↗
It is not a long term limitation. One might design any number of stages to fly in place of Starship on top of the Super Heavy booster.
Also, large science payloads can be launched by SLS. Back in the days of the Ares program, there were proposals to launch an 8 meter reflector (ATLAST-8m)[1] using Ares V. SLS anticipates payloads of such size as well.
So there are at least two viable platforms on which enormous space mirrors might launch, and one of them is likely to be highly cost effective. It's up to the science establishment to propose such missions and get them funded.
[1] <a href="https://ntrs.nasa.gov/citations/20100004890" rel="nofollow">https://ntrs.nasa.gov/citations/20100004890
alexpotato · · focus · HN ↗
B. You could have multiple panels operate as a swarm. There could be many "mirrors" that focus images on one central "collector". That would be larger than any telescope that needs to be shipped as one unit e.g. James-Webb.
grvbck · · focus · HN ↗
Is that level of precision even remotely achievable with today's technology?
My understanding is that orbital insertion accuracy is in the ±10-50 meters range, with the most advanced formation flying satellite swarms hitting 10 cm to 1 m precision between satellites with the help of optical navigation.
But the precision between the panels on a telescope like JWST is in the sub-mm range, no?
Also, I'd assume stuff like orbital decay, atmospheric drag, gravitational perturbations, and solar radiation pressure would make it difficult to maintain precision over time.
I'm sure/hopeful there's some people here at HN working on stuff like this, please fill in and correct me!
ortusdux · · focus · HN ↗
It would be nice to see a swarm of satellites advance astronomy for once!
<a href="https://en.wikipedia.org/wiki/Astronomical_interferometer" rel="nofollow">https://en.wikipedia.org/wiki/Astronomical_interferometer
alexpotato · · focus · HN ↗
The benefit of the "pez dispenser" is that you can very efficiently send up lots of the parts and then deploy them into gigantic arrays.