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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 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 Principal measurement using interferometer and reflective null corrector with CGH 3.75-m M1 fold sphere tilted 14.2° Interferometer interferometer computer-generated hologram CGH of pa rent e llipsi od 25 meters 0.7575-cm m spheremirror Axis Sam GMT segment GMT segment M1 center of curvature Interferometer at M1 center of curvature Test tower at Steward Observatory Mirror Lab Original tower New 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 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 2006-07. Supports all GMT tests, plus LSST, future 6.5 m and 8.4 m mirrors. GMT off-axis segment 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 Cone defined by light from edge of central hole 50 mm CGH compensates only 20µm aspheric departure Vibration insensitive interferometer Optics of Sam Insert a CGH to test Sam Point source microscope aligned to M2 Interferometer for GMT measurements CGH M2 Invar cradle provides stable reference for M2 and CGH 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 M2 mount 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 Interferometer alignment to CGH Use return into interferometer from reference patterns on CGH for • tilt (using fold flat) • shifting interferometer for focus 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 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 3space 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 References co-aligned with CGH CGH, coaligned with: Corner cube tracker reference Flat mirror, angular reference for tracker Alignment error budget Effect on primary mirror segment in telescope correction force (N rms) residual rms surface (nm) 0 2.8 2.4 0.0 0 5.8 5.4 Reference Hologram 0.6 2 6.0 6.9 M1 1.0 5 7.2 9.1 GMT 0.2 0 2.7 3.2 Sam not measured by reference hologram 0.2 3 7.1 7.4 System total 1.2 6 13.4 15.4 radial shift (mm) clocking (arcsec) Interferometer 0.0 M2 3.75 m fold sphere • • • 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 Support of fold sphere 3750 mm mm Hangs from “Active” support, allowing quasi-static force adjustment based on in situ measurement 455 mm Scanning pentaprism test Pentaprism rail lies in plane perpendicular to parent axis. Image at CCD Hub rotates rail to scan different diameters. CCD camera at focus of paraboloid Axis of pa lo rabo id d mate Colli Scanning pentaprism pa rent Fixed reference pentaprism with beamsplitter laser parent paraboloid Off-axis mirror 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. 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 interferometer pentaprism nm rms surface nm rms surface astigmatism 0° 8 9 ± 23 astigmatism 45° 0 -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 aberration interferometric test pentaprism measurement Laser Tracker Plus laser tracker & distance-measuring interferometers (DMI) sphere-mounted retroreflector for laser tracker laser tracker DMI laser and remote receivers PSD 10% BS DMIs DMI retroreflector Retroreflector for interferometer and position sensing detector (PSD) assemblies in 4 places at edge of mirror Poster paper by T. Zobrist et al 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 = 25.497 m) before DMI correction: 1.4 μm rms after DMI correction: 0.75 μm rms 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. 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.