The Telescope of the 2030s
nytimes.com
nytimes.com
"I used to think $10 billion was a lot of money before TARP, the Troubled Asset Relief Program, the $700 billion bailout that saved the banks in 2008 and apparently has brought happy days back to Wall Street. Compared with this, the science budget is chump change, "
[0] https://en.wikipedia.org/wiki/Troubled_Asset_Relief_Program
http://appleinsider.com/articles/15/01/28/by-the-numbers-app...
The U.S. is one rich country. It would be beneficial if we could funnel more money into science. It usually pays dividends.
The problem is the lack of incentives for private funding.
Public funding's issue is that its value, while very real and substantial, is difficult to quantify because it's not in the business of making money. It doesn't deliver a product in the classical sense, it doesn't have a calculated ROI. Improving the lives of humans isn't something an accountant can plot on a spreadsheet.
Public funding is in the business of making new discoveries - many hold little immediate market value but a tonne of value when implemented by private industry years and even decades down the track. That's hard to put a solid number on.
Add to that, private industry leaks money as well. Any sufficiently large organization will require more resources to communicate a policy/directive/goal or pivot than a smaller one. Look at it like an organism - it eats more, wastes more but leaves big tracks in the sand and can attack the bigger problems that smaller organisms can't.
But far more important than that are the drastic changes coming to space launch. Reusability is on the horizon, and innovative launch concepts are being tested. Almost assuredly launch capabilities and launch prices 10 years from now will be very different. And that is the primary driver of cost and program complexity when it comes to orbital space telescopes. High launch costs means that spacecraft need to eek out the utmost performance from within tight payload margins, that raises cost. It means there's no room for contingencies like backup missions, which raises the stakes. And because the cost and stakes are so high that means the vehicle has to be over-engineered so that it has a very high probability of completing its primary mission, which further increases cost. Even though launch doesn't end up being the majority of mission cost, it still has an enormous impact on it.
In a decade or so it may be possible to launch payloads at somewhere between half to 1/10th of current costs. Which opens up a whole new vista of opportunities and changes the local cost/benefit maxima sharply. It will likely be possible to build, launch, and operate a Hubble-class telescope for less than a billion dollars, perhaps only a few hundred million dollars. That makes it more feasible to test innovative designs, it makes it easier to launch a fleet of similar or identical telescopes to increase science throughput, and it makes it feasible to simply replace failed telescopes. That may very well change the way we design and build spacecraft, relying more on extra mass instead of bleeding-edge over-engineering to provide longevity and reliability. But it'll also provide new insights into orbital telescope design, instrumentation, as well as abundant new science data, all of which will inform next generation telescope design, likely leading in different directions from the designs and budgets we would choose today.
The article opens talking about exoplanets rather than very distant galaxies. What does that kind of resolving power - which is deeply impressive - mean for looking at stuff in our immediate neighborhood?
I wonder if the thin atmosphere or moon-quakes make this non optimal.
It also doesn't make sense to geosync the telescope behind the "dark side" of the earth for the same reason. Long exposures wouldn't be easy since the earth does move around the sun, so the sky moves with it. Eventually you will have to face the sun to get the same shot of the sky.
So, the only way would to be to have the orbit around the sun so the telescope can always face away from the sun. that way you can at least create the long exposures they need.
The linked report also answers the "why there" question I immediately had.
> The HDST spacecraft and its operations will likely share many commonalities with the JWST architecture and operations. For HDST, as for JWST, an L2 halo orbit is preferable to a geosynchronous orbit (and most others, including low-earth orbit), because it is thermally stable and has lower fuel requirements for station-keeping
https://static1.squarespace.com/static/558adc44e4b002a448a04...
(if that link expires, it was from here: http://www.hdstvision.org/report )