html5-img
1 / 23

Fabrication and testing of KGMT FSM prototype

Fabrication and testing of KGMT FSM prototype. Ho-Soon Yang, Hak-Yong Kihm, Il-Kwon Moon, Jae-Bong Song, Yun-Woo Lee Korea Research Institute of Standards and Science, Korea Young-Soo Kim Korea Astronomy & Space Science Institute, Korea. Oct. 4. 2010. Contents. Objective of project

tolla
Download Presentation

Fabrication and testing of KGMT FSM prototype

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Fabrication and testing of KGMT FSM prototype Ho-Soon Yang, Hak-Yong Kihm, Il-Kwon Moon, Jae-Bong Song, Yun-Woo Lee Korea Research Institute of Standards and Science, Korea Young-Soo Kim Korea Astronomy & Space Science Institute, Korea Oct. 4. 2010

  2. Contents Objective of project Recent experiences in KRISS Manufacturing flow diagram Optical testing Working cell design Future works

  3. Objective • Technology development related to manufacturing of FSM for GMT project in advance • For FSMP • Use a model very close to FSM  FSM prototype in KGMT project • Fabrication of FSMP with its own working cell designed by KRISS • Optical testing of FSMP after assembly with a cell (very close to real FSM cell)

  4. Recent experiences @ KRISS • 800 mm lightweighted mirror for space application (1/2) Gravity Quilting (30 g/cm2) And other environmental effects …

  5. Recent experiences @ KRISS • 800 mm lightweighted mirror for space application (2/2) • - Measurement of wavefront error with two different methods : • CGH (computer generated hologram) and conventional null lenses /30 rms CGH Conventional null lens

  6. Recent experiences @ KRISS • 1 m off-axis paraboloid for collimator (1/2) • - Focal length = 6 m • - Distance between the center of OAP and optical axis = 700 mm Flat mirror OAP Interferometer

  7. Recent experiences @ KRISS • 1 m off-axis paraboloid for collimator (2/2) OAP mirror Alignment telescope Interferometer Reference flat

  8. Fabrication facilities in KRISS Measuring tower with null interferometer Rotating table with aspheric surface under test 1 m polishing machine 2 m polishing machine 2 m coating chamber Assembly room 2 m CNC machine 0.6 m polishing machine & testing tower

  9. Manufacturing flow diagram 10% larger size Mirror blank procurement Curve generation Lightweighting Chemical Etching Rounding to target dimension Inspection Polishing Grinding Figuring (98%) Final figuring Inspection Assembly with cell Inspection FAT

  10. Scheme of Optical testing • Efficient testing process is a key for successful fabrication of mirror Grinding Polishing Figuring Spherometer Profilometer ~ mm Profilometer Interferometer ~ μm Interferometer with CGH ~ nm

  11. KRISS profilometer • Measurement accuracy ~ 1 um • Compensation of measurement errors of probe system using a high quality reference mirror Reference mirror

  12. Interferometric testing using CGH 3 2 1 150 mm 4 CGH layout : (Line spacing : ~ 20 um) Adjustment between interferometer and CGH Test configuration of FSMP off-axis segment (off-axis type CGH )

  13. CGH alignment 3 Adjustment I between CGH and FSMP segment 2 1 4 Adjustment II between CGH and FSMP segment

  14. Testing tower setup KRISS Profilometer Turn-over tool

  15. Testing configuration Optical testing after assembly with FSMP cell Optical testing during fabrication

  16. Concept for working cell design Minimization of print through Load cell on the back plate of the mirror 24 axial support location Polishing pressure at the pocket of mirror with 0.1 psi

  17. FE Model of M2 Top view bottom view Thin shell elements Material : Zerodur Diameter : 1064 mm Thickness : 140 mm Hole size : 100 mm Mass : 94 kg Face sheet : 20 mm Back plate : 14 mm Rib : 5 mm Web : 10 mm

  18. Axial support y x Support locations

  19. Print through Surface error Without correction PV 166 nm RMS 48 nm Surface error With correction PV 50 nm RMS 9 nm Displacement PV 165 nm Gravity z

  20. Print through M2 structure function Gravity z

  21. Surface error Surface error Without correction PV 110 nm RMS 31 nm Surface error With correction PV 35 nm RMS 6 nm Displacement PV 110 nm Quilting effect from polishing pressure of 0.1 psi

  22. Surface error M2 structure function Polishing pressure 0.1 psi

  23. Future works • Manufacturing of two types of CGH • Manufacturing of testing tower • Optimization of mirror working cell • Fabrication of FSMP by the end of next year • We hope to take parts in the fabrication of FSM in future

More Related