2015
DOI: 10.1088/0264-9381/32/15/155011
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Performance test of pipe-shaped radiation shields for cryogenic interferometric gravitational wave detectors

Abstract: One of the most important challenges in cryogenic interferometric gravitational wave detectors is to reduce the undesirable thermal radiation coming through holes in the radiation shield, which are necessary for the laser beam to pass through. For this purpose, pipe-shaped radiation shields called duct shields are used. Here, we have manufactured duct shields for KAGRA in Japan, one of the cryogenic interferometric gravitational wave detectors, and measured the thermal radiation coming through the duct shields… Show more

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Cited by 19 publications
(11 citation statements)
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“…Cold Shields To minimize the radiative heat load from the 300 K beam tube, the radiation shield will need to include a cylindrical piece which extends into the beam tube. The inside of the shield will require baffles, as in the KAGRA design, to reduce multiple reflection paths from the 300 K environment [132]. The inside of the long shield should be coated with a high emissivity black coating to maximize the radiative coupling to the test mass.…”
Section: A2 Radiative Cooling Of the Test Massmentioning
confidence: 99%
“…Cold Shields To minimize the radiative heat load from the 300 K beam tube, the radiation shield will need to include a cylindrical piece which extends into the beam tube. The inside of the shield will require baffles, as in the KAGRA design, to reduce multiple reflection paths from the 300 K environment [132]. The inside of the long shield should be coated with a high emissivity black coating to maximize the radiative coupling to the test mass.…”
Section: A2 Radiative Cooling Of the Test Massmentioning
confidence: 99%
“…Moreover, in order to accelerate the cooling time, it is planned to coat all the payload (with the exception of the mirror, of course) with diamond like carbon (DLC). According to the simulations this solution allows increasing the radiation cooling efficiency and thus reducing the total cooling time from nearly two months to 39 d. Experimental tests done with a half size prototype of the payload coated with DLC confirmed the validity of the simulation [129].…”
Section: The Kagra Solutionsmentioning
confidence: 59%
“…This design should allow to extract the amount of power deposited by the laser in the mirrors and cool down the mirror to 20 K provided a sufficiently heat conduction path is made between the mirror and the cryo-coolers. In addition two 5 m long cryogenic ducts allow the laser beam to enter the cryostat and while reducing the 300 K radiation input to the mirror by a factor of a thousand compared to the input one would have from the tube in the absence of the ducts [129].…”
Section: The Kagra Solutionsmentioning
confidence: 99%
“…The cryostat for the test masses also have various kinds of baffles for absorbing stray light inside the cavity, and duct shields at both sides for absorbing the room temperature thermal radiation from vacuum ducts [23,24]. We use four low vibration double-stage pulse-tube cryocoolers for each cryostat [25,26].…”
Section: Interferometer Configuration Of Bkagramentioning
confidence: 99%