Why can't we build a huge stationary optical telescope inside a depression similar to the FAST?
Of course @ProfRob's answer is correct. If the crater were on Earth under Earth's atmosphere you'd have to probably build a zillion segments and use standard adaptive optics to both:
- maintain exact phase relationship between all of the segments located so far from each other
- constantly correct for astronomical seeing effects.
However, you could kill two birds with one stone by building in a giant crater on a low gravity body like the Moon at 0.16 g, or even Ceres at 0.03 g.
I don't know if you could get to even 200 meters right away, but the 2nd or 3rd iteration might do it if there was some reason to.
Inside the crater you would build a support for the mirror, but you'd really be supporting a race track to hold a concave basin in which a liquid compatible with vacuum would be added.
If you spin it fast enough, the liquid will climb the walls and assume a parabolic shape with a thickness of order a millimeter, and smooth out the imperfections in the support.
This is where low gravity comes in; the lower the gravitational acceleration, the lower angular rate at which you'd need to spin it.
The mirror technology described in Angel et al. 2008 is a spinning thin layer of an organic ionic liquid on to which is evaporated a thin silver surface. There is no spinning mercury in this proposed instrument, to be built on one of the poles of the Moon.
Abstract
We have studied the feasibility and scientific potential of zenith observing liquid-mirror telescopes having 20-100 m diameters located on the Moon. They would carry out deep infrared surveys to study the distant universe and follow up discoveries made with the 6 m James Webb Space Telescope (JWST), with more detailed images and spectroscopic studies. They could detect objects 100 times fainter than JWST, observing the first high-redshift stars in the early universe and their assembly into galaxies. We explored the scientific opportunities, key technologies, and optimum location of such telescopes. We have demonstrated critical technologies. For example, the primary mirror would necessitate a high-reflectivity liquid that does not evaporate in the lunar vacuum and remains liquid at less than 100 K. We have made a crucial demonstration by successfully coating an ionic liquid that has negligible vapor pressure. We also successfully experimented with a liquid mirror spinning on a superconducting bearing, as will be needed for the cryogenic, vacuum environment of the telescope. We have investigated issues related to lunar locations, concluding that locations within a few kilometers of a pole are ideal for deep sky cover and long integration times. We have located ridges and crater rims within 0.5° of the north pole that are illuminated for at least some sun angles during lunar winter, providing power and temperature control. We also have identified potential problems, like lunar dust. Issues raised by our preliminary study demand additional in-depth analyses. These issues must be fully examined as part of a scientific debate that we hope to start with the present article.
A telescope capable of reaching these limits has been
proposed, for example, by Angel et al. (2008) in the form
of a cryogenic liquid-mirror telescope on the surface of
the moon. However, as the authors mention, a liquid
mirror might face some challenges, as it is unclear what
effect lunar dust would have on the instrument and the
observations.
To avoid an articulating mount, the telescope would
be placed at the lunar pole, constantly pointing at the
zenith. To assure thermal isolation, it would be located
in the permanent shadow in a lunar crater. The limit
on exposure time is then given by the precession of the
moon, and is of the order of several days. This can
only be extended by the addition of some active tracking facility, for example a moving prime focus platform.
However, to reach the sensitivities we require, a mirror diameter of 100 m is necessary. We note that Angel
et al. (2008) do consider mirror sizes of 20 up to 100 m
in their preliminary design studies. While 100 m is evidently challenging, it is within the realm of possibility
for mid-century technology.
How do non-metallic liquid telescope mirrors remain as liquid in the vacuum of space?
The proposed mirror uses an ionic liquid rather than a real liquid metal (e.g. mercury or some other eutectic). Nobody balks as using mercury because it might evaporate, because we have some sense that at low temperatures (e.g. room temperature) those of us who are old enough might have played with a bit in school presumably in a glass dish or at home from a broken thermometer, and remember that it just sits there; it doesn't boil away and nobody was worried about breathing vapor from it.
That's because the vapor pressure of mercury at room temperature is only of order $3 \times 10^{-7}$ atmospheres and the evaporation rate is low. We would not do such things today, but we have at least seen images if liquid mercury in air and don't think of it as evaporating quickly, and have heard of spinning mercury telescopes and mercury based barometers with one end exposed to atmosphere.
Going even somewhat below room temperature the vapor pressure and evaporation rates of mercury plummets.
It turns out that ionic liquids even those based on organic molecules can have similarly low vapor pressures in the regime below room temperature and above their freezing points.
An ionic liquid (IL) is a salt in the liquid state. In some contexts, the term has been restricted to salts whose melting point is below some arbitrary temperature, such as 100 °C (212 °F). While ordinary liquids such as water and gasoline are predominantly made of electrically neutral molecules, ionic liquids are largely made of ions and short-lived ion pairs. These substances are variously called liquid electrolytes, ionic melts, ionic fluids, fused salts, liquid salts, or ionic glasses.
So because their constituents hold each other due to strong ionic forces, many of these liquids can have very low vapor pressures and evaporation rates at room temperature and even lower at reduced temperatures still above their freezing points. These temperatures are readily available in space environments; as long as sunlight is appropriately shielded, radiative cooling to space allows access to cryogenic environments.
Angel et al. 2008 says:
Borrowing from techniques used to coat solid mirrors on Earth, we conducted a
number of experiments coating a variety of liquids by vaporizing silver on their surfaces. A recent article (Borra et al. 2007) summarizes our recent efforts. We successfully coated an ionic liquid with silver. Coating an ionic liquid was a major breakthrough because ionic liquids have negligible vapour pressures and thus do not evaporate in vacuum. We experimented with a commercially available ionic liquid that solidifies at 175 K and we are actively pursuing ionic liquids with lower freezing temperatures. There is a realistic expectation of success because ionic liquids are organic compounds and there are at least 106 simple ionic liquids, and 1018 ternary ionic liquid systems (Borra et al. 2007), giving a phenomenally wide choice for optimizing the properties of the liquid substrate.
Borra et al. 2007 can be found in Nature: Deposition of metal films on an ionic liquid as a basis for a lunar telescope and also accessed in researchgate
click images for larger size
left: "Figure 1. Experimental vapor pressure data for mercury." Source: NIST Internal Report The Vapor Pressure of Mercury NISTIR 6643 (also here) and right: Source Don't do this!
See MIT's discussion of the dangers of mercury exposure in Mercury