A deployable, annular, 30m telescope, space-based observatory [pdf]
northropgrumman.com
northropgrumman.com
Why wrong? This is a project proposed by Northrop Grumman, a defense company. It would be wrong for them to look at the stars, rather than down to Earth.
This proposed mirror is a foil of zirconium copper that is sputtered onto a glass mandrel and then epoxied to a silicon carbide Isogrid. The advantage is you only have to accurately polish the one glass mandrel, the substrate need not be super accurate.
Anyone know if this method is really better than using solid beryllium, or is this just Northrop Grumman marketing?
The abstract at least doesn’t mention IR observation, in eg visible spectrum JWST would surely be built differently (more cheaply).
EDIT in fact they do reference JWST but I guess only as a point of comparison, as it does have a large mirror. Their parameters table shows observations would be in visible spectrum (450-750nm).
Hubble is an unshaded warm-mirror telescope that can observe down to 1700nm, though, so I wonder why they wouldn't use that as comparison.
Also, I wonder since the L2 spot is theoretically (partly) shaded by the earth, how much Watts/m^2 do you avoid ?
Hubble used cooled instruments, warm mirror. If you only partially cool a mirror then thermal expansion effects will mess up the focus. In the paper they propose heating segments that are shadowed, to keep the whole mirror at the same temp.
Be is lower density, which would matter for payload mass. The SiC material has a much lower thermal expansion coefficient and change of CTE with temperature, both of which should reduce thermal deformation.
[1] https://www.northropgrumman.com/wp-content/uploads/CERAFORM_...
These are huge beasts with dishes of 100 meters in the previous generation of MAGNUM satellites and over 100 meters in the latest MENTOR satellites… of course these numbers are based on the usual educated rumour mill sources necessary with any spy satellite information that has yet to be declassified, and the entire SIGINT family of satellites going right back to almost the very first is as black as pitch, it’s code name only educated guesswork and a couple of rare leaks of surprisingly inconsequential information. But the dish sizes are one of the more consistent bits of information so it’s a fairly safe bet these lower bound numbers are accurate.
Maybe put them on independently orbiting satellites that station-keep with ion rockets. Or, in a space frame formed of nanowires, with the nodes individually charged electrically to repel one another, maintaining the wires in tension.