magellan f/15 chopping secondary magellan sac meeting laird close (principle investigator)
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Magellan F/15 Chopping Secondary Magellan SAC Meeting Laird Close (Principle Investigator) Victor Gasho (Program Manager) September 24, 2005. Project Overview. Develop Magellan f/15 Chopping Tip-Tilt secondary Si clad SiC Mirror - PowerPoint PPT PresentationTRANSCRIPT
1September 24, 2005 Magellan F/15 Chopping Secondary
Magellan F/15 Chopping Secondary
Magellan SAC Meeting
Laird Close (Principle Investigator)
Victor Gasho (Program Manager)
September 24, 2005
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Project Overview• Develop Magellan f/15 Chopping Tip-Tilt secondary
–Si clad SiC Mirror
•Lightweight (~8 kg) using egg-crate rib structure and thin face-sheet
•Very Stiff (~900Hz)
• Low CTE (2ppm/C)
• High thermal conductivity (better than aluminum)
– Physik Instrumente HVPZT Tip/Tilt/Chop Stage
•Capable of 2 Axis chopping
•Reactionless (98% Goal)
• High speed (~1 kHz)
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Brief Project History1) From the beginning it was
recognized that Magellan needed a low emissivity secondary mirror. Factor of ~3 gain in exposure time possible for Mid-IR science at Cass.
2) A conceptual design was made ~1995, and contract placed with Lockheed to produce a tip-tilt chopping SiC secondary for ~900k$.
3) Polished Reaction Bonded SiC was found rougher than ~100A rms --project canceled.
4) In 2002 a 1.3 M$ NSF MRI award (PI Close) was made to provide Magellan with an adaptive secondary with tip-tilt capabilities to be provided in the funded phase 1. Full AO was to be provided at a later date from another unidentified grant.
5) Applications for enough money to finish & commission the AO secondary were turned down by AODP (twice) and TSIP (once). No further funds identified at this point.6) NSF has denied year 3’s funding due to risk, cost, & management. NSF expects SAC decision on a successful approach by end of Sept. NSF approved CDR required in fall.7) On the Sept 9, 2005 the SAC unanimously directed Close & Gasho to pursue a lightweight f/15 tip-tilt chopping secondary and not continue with the adaptive secondary.8) Here is an overview of how we can accomplish the original goals of a low emissivity tip-tilt chopping secondary for MIRAC4 and deliver the funded MRI science (and optical speckle).
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Preliminary Specs of Mirror
Material Si Clad Silicon Carbide
Diameter 641.47 mm
Mirror Mass ~8.0 kg
Mirror Surface Error 40 nm rms
Mirror Surface Roughness 20 Å rms
Support Mass ~160 kg
Mirror Moment of Inertia @ CG ~0.30 kg/m2
System Resonance Frequency >300 Hz
Chopping Movement +/- 45” sky @ 0.5 Hz
+/- 16” sky @ 2Hz
+/- 3.5” sky @ 10Hz
Tip/Tilt Movement +/- 0.5” sky @ 100Hz
Angular Resolution 0.010” sky
Chopping Mechanism HVPZT Reactionless
Coating Gemini Silver?
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MIRAC 4 and f/15 Secondary Mounted
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F/15 Secondary Swing ArmSwing Arm
•Allows for fast deployment.
•Borrowed from previous Magellan f/15 design.
•When in retracted position will intrude in aperature and block 0.15% light.
•Trade off of optical performance vs operational needs.
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F/15 Secondary Assembly
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F/15 Secondary SiC Mirror
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PI Stage Chopping Simulation
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Examples of Chopping Secondaries
• IRTF (Infrared Telescope Facility)• Mirror diameter: 244 mm (SiC)• Tip/Tilt range: ±250 µrad (PI PZT) • 10 Hz chopping• Resonant frequency: 490 Hz
• SOFIA• Mirror diameter: 350 mm (SiC)• Tip/Tilt range: ±10 mrad (CSEM Voice Coil)• 20 Hz chopping• Resonant frequency: 422 Hz
• UKIRT (United Kingdom Infra-Red Telescope)• Mirror diameter: 314 mm (Zerodur)• Tip/Tilt range: ±500 µrad (PI PZT)• Resonant frequency: 280 Hz • 6 Hz chopping
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Example of Large Si Clad SiC Mirror
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MIRAC and Tip Tilt Camera
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Camera and Optics
~100” MIRAC FOV (~60mm Optics)
25 mm travel x-y stage (0.3 m accuracy)
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Tip/Tilt Camera
• Andor iXon DV-860 Camera
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Schedule
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•Questions?