ID |
Date |
Author |
Type |
Category |
Subject |
1
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Wed Jan 2 12:06:43 2019 |
Dennis Coyne | General | General | Current status/state of the Optical Contamination Facility (formerly OTF) | The Optical Contamination Facility (formerly the OTF, Optical Test Facility) consists of 3 vacuum chambers with high-finesse, resonant optical cavities used to test the effect of outgassing from materials/assemblies on optical properties (absorption, scatter @1064nm) over time.
basic description: P990032
original block diagram: D1001800
new block diagram: D1800215
compendium of all materials/assemblies tested to date (includes RGA results as well): E1000193
Current facility status:
- One of the cavities is currently not operating until we get another NPRO laser.
- Currently only one test is underway - vacuum compatibility of the EUCLID device; see E1800210
- Current materials test queue (in my ordering of priority):
- EUCLID (possible A+ component) - testing underway
- Accu-Glass PEEK UHV Heat-Shrink Tubing (useful for in-chamber cabling)
- Krytox LVP (not officially approved for LIGO, but permitted extremely small amounts on beam diverters & within New Focus picomotor 830X-UHV)
- Torr Seal epoxy (proposed for ZnSe window seal for in-vacuum, non-pumped, wavefront sensor by Australians, possibly for A+?)
- Castrol Braycote 601EF (used in a proposed vacuum rated heat switch motor assembly for Voyager)
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3
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Tue Feb 19 09:35:33 2019 |
Dennis Coyne | Plan | General | OCF Queue | Here is an update to the prioritized materials testing queue for UHV compatibility, which was last reported in elog:1
- NKT Photonics large mode area, Photonic Crystal Fiber (PCF) ESM-12B sourced from ThorLabs. This is a fiber under consideration for higher power, lower loss, green light injection for the OPO in the squeezer subsystem. (High priority due to degradation of the H1 fiber.)
- Accu-Glass PEEK UHV Heat-Shrink Tubing (useful for in-chamber cabling)
- Krytox LVP (not officially approved for LIGO, but permitted extremely small amounts on beam diverters & within New Focus picomotor 830X-UHV)
- Torr Seal epoxy (proposed for ZnSe window seal for in-vacuum, non-pumped, wavefront sensor by Australians, possibly for A+?)
- Castrol Braycote 601EF (used in a proposed vacuum rated heat switch motor assembly for Voyager)
Note that the following test has been terminated/completed:
- E1800210, EUCLID (possible A+ component) - failed (marginally) after 215 days of testing
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4
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Tue Feb 25 14:02:17 2020 |
Dennis | Progress | General | Optical Contamination Cavity Testing Queue | Here is an update to the prioritized materials testing queue for UHV compatibility, which was last reported in elog:3
- On-going test - can be terminated now: E1900220-v1: Optical Contamination Test results: SR3 ROC Actuator, Ceramic Heater Assy
- On-going test - some value in continuing test: E1900232-v1: Optical Contamination Test results: Low-Reflection, Matte Black Aluminum Foil
- Accu-Glass PEEK UHV Heat-Shrink Tubing (useful for in-chamber cabling)
- Krytox LVP (not officially approved for LIGO, but permitted extremely small amounts on beam diverters & within New Focus picomotor 830X-UHV)
- Torr Seal epoxy (proposed for ZnSe window seal for in-vacuum, non-pumped, wavefront sensor by Australians, possibly for A+?)
- Castrol Braycote 601EF (used in a proposed vacuum rated heat switch motor assembly for Voyager)
Note that the following test has been terminated/completed "recently":
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2
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Thu Jan 17 16:04:17 2019 |
Dennis Coyne | General | General | revised thermoelastic response of the cavity mirror | The original thermoelastic response of the mirror was documented in T970212, using the IDEAS finite element code. The analysis was redone using ANSYS and an analytical (series expansion); These two approaches agree with each other fairly well. The new results are similar to the original steady-state calculations in the original T970212-x0. The new results are uploaded to T970212-v1. While the characteristic time for the thermal response of the mirror (assuming only radiative coupling, no conduction) is ~190 sec (~3 minutes), the thermal response and thermoelastic deflection are at 90% of the steady-state value in ~30 seconds.
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