Presentation is loading. Please wait.

Presentation is loading. Please wait.

J. H. Burgea,b, W. Davisona, H. M. Martina, C. Zhaob

Similar presentations


Presentation on theme: "J. H. Burgea,b, W. Davisona, H. M. Martina, C. Zhaob"— Presentation transcript:

1 Development of surface metrology for the Giant Magellan Telescope primary mirror
J. H. Burgea,b, W. Davisona, H. M. Martina, C. Zhaob aSteward Observatory, University of Arizona bCollege of Optical Sciences, University of Arizona

2 GMT primary mirror segments
25 meter telescope, requires 7 mirror segments Each mirror segment is 8.4 meters in diameter The off axis segments have 14.5 mm aspheric departure

3 Principal measurement using interferometer and reflective null corrector with CGH
Interferometer at M1 center of curvature

4 Test tower at Steward Observatory Mirror Lab
New tower Original tower New tower 28 meters tall, 80 tons of steel floated on 400 ton concrete pad accommodates other UA projects (LBT, LSST) lowest resonance of 4.8 Hz with 9 ton 3.75-m fold sphere + cell

5 New test tower at Mirror Lab
Test optics for GMT segment Test of 3.75 m fold sphere 28 m vibration-isolated tower was installed Supports all GMT tests, plus LSST, future 6.5 m and 8.4 m mirrors. GMT off-axis segment

6 Measurement of center segment
The center segment can be measured by tilting the fold sphere to point straight down, then a small computer generated hologram will compensate the residual errors. Cone defined by light from outer edge of mirror 50 mm CGH compensates only 20µm aspheric departure Cone defined by light from edge of central hole Vibration insensitive interferometer

7 Optics of Sam ~1.5 m CGH M2 Insert a CGH to test Sam
Point source microscope aligned to M2 ~1.5 m Interferometer for GMT measurements CGH M2

8 Invar cradle provides stable reference for M2 and CGH

9 M2 is aligned to CGH Point Source Microscope M2 CoC reference ball M2 CoC reference ball To M2 Computer generated hologram CGH and M2 CoC reference ball are aligned using CMM to 10 µm M2 aligned to CoC reference ball using PSM

10 M2 mount

11 Use of a Point Source Microscope to align M2
Use cradle to locate ball at location where M2 center of curvature should be (cradle geometry defined by CMM) PSM is adjusted to the ball The ball is then removed. The PSM is looking at mirror directly. Adjust the mirror until reflection from it is focused on the same spot as the ball on the camera

12 Interferometer alignment to CGH
Use return into interferometer from reference patterns on CGH for tilt (using fold flat) shifting interferometer for focus

13 CGH test of Sam CGH inserted into light coming from Sam
Reflection back through system is used to verify wavefront CGH mounted on invar plate with other references for M1 alignment

14 Alignment of M1, GMT M1 is aligned to Sam with ~100 µm tolerances
Reference hologram is aligned to Sam. Then it is used to represent Sam. A laser tracker measures the 3-space position of the reference hologram and M1. M1 is aligned to the reference hologram according to the measurements. The laser tracker also provides the reference for the GMT location in the test

15 References co-aligned with CGH
CGH, coaligned with: Corner cube tracker reference Flat mirror, angular reference for tracker

16 Alignment error budget
Effect on primary mirror segment in telescope radial shift (mm) clocking (arcsec) correction force (N rms) residual rms surface (nm) Interferometer 0.0 2.8 2.4 M2 5.8 5.4 Reference Hologram 0.6 2 6.0 6.9 M1 1.0 5 7.2 9.1 GMT 0.2 2.7 3.2 Sam not measured by reference hologram 3 7.1 7.4 System total 1.2 6 13.4 15.4

17 3.75 m fold sphere Cast in the Mirror Lab spinning oven
Figure of fold sphere will be measured in situ and subtracted. Accuracy of correction depends on slope errors, and magnitude of small-scale structure that cannot be subtracted. Finished fold sphere meets requirements: < 2 nm/cm rms slope error small-scale errors < 15% of GMT segment specification Overall accuracy < 20 nm rms over clear aperture. Cast in the Mirror Lab spinning oven Polished at the Mirror Lab Coated at Kitt Peak

18 Support of fold sphere 3750 mm mm 455 mm mm Hangs from “Active” support, allowing quasi-static force adjustment based on in situ measurement

19 Scanning pentaprism test
Pentaprism rail lies in plane perpendicular to parent axis. Hub rotates rail to scan different diameters. Scanning pentaprism measures slope errors by producing collimated beams parallel to parent axis. Displacement of focused spot is measured with camera in focal plane. Scanning pentaprism test as implemented for GMT off-axis segments. Pentaprism rail is suspended from tower.

20 Pentaprism test of 1.7 m off-axis NST mirror
1/5 scale GMT pentaprism test This was done in late 2007 before the mirror was finished. The pentaprism test only samples lowest order aberrations The PP results agree with results from interferometry Poster paper by P.Su et al pentaprism measurement interferometric test aberration interferometer pentaprism nm rms surface astigmatism 0° 8 9 ± 23 astigmatism 45° -2 ± 23 coma 0° -87 -98 ± 12 coma 90° -4 16 ± 12 trefoil 0° -50 -32 ± 35 trefoil 30° 9 23 ± 30 spherical -32 -35 ± 8 nm surface

21 Laser Tracker Plus Poster paper by T. Zobrist et al
laser tracker & distance-measuring interferometers (DMI) sphere-mounted retro-reflector for laser tracker laser tracker DMI laser and remote receivers PSD 10% BS DMIs Retroreflector for interferometer and position sensing detector (PSD) assemblies in 4 places at edge of mirror DMI retroreflector Poster paper by T. Zobrist et al

22 Laser Tracker Plus measurement of 3.75 m fold sphere M1
R = 25.5 m, tracker distance = 22 m 93 sample points, measured 4 DMIs with each sample Subtracted best-fit sphere (R = m) before DMI correction: 1.4 μm rms after DMI correction: 0.75 μm rms

23 Shear test Each segment has axisymmetry about parent axis
Rotate segment about this axis under the optical test and separate effects that move with the mirror from those that remain with the test.

24 Summary We are building the hardware to measure the GMT segments. We expect to meet a tight error budget Low order modes controlled by active optics, using < 5% Force Uncorrectable features fit well within the allotted GMT PM structure function We take this problem seriously and have implemented a comprehensive set of crosschecks Scanning pentaprism system Laser tracker Plus Shear test We have invested in metrology for making the first of the segments. Others will be made at low risk, low cost.


Download ppt "J. H. Burgea,b, W. Davisona, H. M. Martina, C. Zhaob"

Similar presentations


Ads by Google