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Cryo-payload Kazuhiro Yamamoto Institute for Cosmic Ray Research

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Presentation on theme: "Cryo-payload Kazuhiro Yamamoto Institute for Cosmic Ray Research"— Presentation transcript:

1 Cryo-payload Kazuhiro Yamamoto Institute for Cosmic Ray Research
The University of Tokyo KAGRA face to face meeting University of Toyama, Toyama, Japan 27 August 2015

2 0. Abstract Here, I explain (1) Current status and next step
(2) Human resources for cryogenic payload 2

3 Contents Introduction Sapphire suspension Cryogenic payload
Human resources Summary 3

4 1. Introduction Schematic view of KAGRA interferometer
Four mirrors of arm cavity will be cooled. 3km 3km Mozumi Y-end Sakonishi X-end Kamioka mine (Underground site) Atotsu Center Vibration isolation system (Type A), Cryocooler unit, Cryostat, Cryogenic payload 4 4 4 4 4 4 4 4

5 Vibration isolation system Vacuum ducts along laser beam
1. Introduction Outline of vibration isolation and cryostat Design drawing with tunnel and cross section 2nd floor A. Hagiwara Vibration isolation system (room temperature) 14 m Shaft Clean booth Vacuum ducts along laser beam Cryostat (Here is a mirror) 5 5 5

6 1. Introduction Schematic view of cryo-payload Sapphire suspension
Pulse tube cryocoolers Pulse tube cryocoolers Sapphire fiber Cryo-payload Sapphire mirror (About 20K)

7 2. Sapphire suspension Sapphire lop-eared suspension
“Sapphire monolithic lop-eared suspension” One of the most important parts of KAGRA : Main sapphire mirrors are included. All parts are made from sapphire. fiber break Hydroxide Catalysis Bonding 7

8 2. Sapphire suspension Current status
We investigated almost all components. We must construct full size suspension (prototype). 8

9 2. Sapphire suspension All sapphire parts for full size prototype have already been delivered. Jigs for assembly is being prepared. Sapphire cylinder with flat cuts as dummy mirror Fibers with nail head Blade spring Ears 9 9 9 9 9 9 9 9

10 3. Cryogenic payload Outline of vibration isolation and cryostat
Heat link (pure Al) Heat link (pure Al) Pulse tube cryocoolers Pulse tube cryocoolers Cryo-payload 10 10 10 10 10 10 10

11 3. Cryogenic payload Outline of cryogenic payload Platform Marionetta
Recoil mass chain (Thermal noise caused by this part is small) Marionetta Intermediate mass Sapphire Mirror 11 11 11 11 11 11 11

12 3. Cryogenic payload Outline of cryogenic payload GAS filer Platform
for vertical vibration isolation (Mirror chain is suspended) Platform Marionetta Intermediate mass Recoil mass chain Sapphire Mirror 12 12 12 12 12 12 12

13 3. Cryogenic payload Outline of cryogenic payload Platform
Alignment adjustment system Platform Marionetta Simple system for high Q-value of sapphire suspension Intermediate mass Sapphire Mirror 13 13 13 13 13 13 13

14 3. Cryogenic payload Outline of cryogenic payload Platform
Sensor and actuator (for control and damping) Marionetta Intermediate mass Sapphire Mirror Recoil mass chain 14 14 14 14 14 14 14

15 3. Cryogenic payload Current status A. Hagiwara proceeds with
CAD design drawings. Almost all parts except for platform were designed. Design is based on discussion with VIS (9 Mar. 2015) Platform Marionetta Intermediate mass Mirror Recoil mass A. Hagiwara 15 15

16 3. Cryogenic payload Current status A. Hagiwara proceeds with
CAD design drawings. Almost all parts except for platform were designed. Recoil mass for Marionetta Recoil mass for intermediate mass Recoil mass for mirror A. Hagiwara 16 16

17 3. Cryogenic payload Next step Prototype test of cryogenic payload
Two differences from actual one Platform does NOT include GAS filter. Mirror and fibers are NOT made from sapphire, but metal. 17

18 3. Cryogenic payload 23 kg 150 mm 220 mm
Prototype test of cryogenic payload Dummy mirror and ears (stainless) Size and weight are the same as those of KAGRA mirror. 23 kg 150 mm 220 mm Ears (stainless) Recoil mass 18 18 18 18 18 18 18

19 3. Cryogenic payload Prototype test of cryogenic payload
Dummy blade spring Marionetta Intermediate mass 19 19 19 19 19 19 19

20 3. Cryogenic payload Prototype test of cryogenic payload 20

21 4. Human resources 8 scientists 2 graduate students (Master course)
3 technical staffs 21

22 KAGRA Cryogenics Group
2015.Jul.25 Takayuki TOMARU Chief KEK, Assoc. Prof. Toshikazu SUZUKI EO and SEO member KEK, Senior Fellow Nobuhiro KIMURA Cryostat sub-chief KEK, Assoc. Prof. Tatsuya KUME Surveying, Alignment KEK, Assoc. Prof. Kazuhiro YAMAMOTO Cryo-Payload sub-chief ICRR, Project Assist. Prof. Suguru TAKADA Cryogenics NIFS, Assist. Prof. Rahul KUMAR Simulation, Payload KEK, PD Kieran CRAIG Payload ICRR, PD Hiroki TANAKA Cryo-Payload, Q ICRR, Grad. Student Takahiro MIYAMOTO Cryo-Payload ICRR, Grad. Student By T. Tomaru (Revised by K. Yamamoto) Shinichi TERASHIMA Machining KEK, Technical Staff Ayako HAGIWARA CAD KEK, Technical Staff Iwao MURAKAMI Welding, Assembly KEK, Technical Staff 22

23 4. Human resources Kieran Craig (from Glasgow) starts to work as postdoc in ICRR on the 1st of August ! Ph.D. defense was on last July ! “Studies of the mechanical dissipation of thin films for mirrors in interferometric gravitational wave detectors” 23

24 5. Summary Full size prototype at KEK and ICRR Cryogenic payload (KEK)
Parts of mirror chain were assembled. Design of recoil mass chain and platform is in progress. Sapphire lop-eared suspension (ICRR) Assembly jig are being prepared. 2. Human resource Kieran Craig (Post doc) joins our team ! 24

25 Thank you for your attention !
25

26 Backup 26

27 6. Summary Next step (by Spring 2016)
Full size prototype at KEK and ICRR 2. By Spring 2017 Development of platform (GAS filter) By Summer 2017 Assembly and test of sapphire suspension In the second half of 2017 Installation at KAGRA site One postdoc joins one week later. KAGRA must take care of KEK people. Otherwise, they can not work for KAGRA after 2018. 27

28 3. Sapphire suspension Schedule By Spring 2016 : Prototype test
of full size sapphire suspension at ICRR By Autumn 2016 : Procurement of sapphire parts By Spring 2017 : Assembly and test with End sapphire mirrors By Summer 2017 : Assembly and test with Front sapphire mirrors By End 2017 : Installation at KAGRA site 28

29 3. Cryogenic payload Schedule By Spring 2016 : Prototype test
of full size prototype at KEK By Spring 2017 : Development of platform (GAS filter) By End 2017 : Installation at KAGRA site 29

30 4. Schedule 30

31 4. Schedule Full size prototype at KEK and ICRR
Procurement of sapphire parts Assembly and test of sapphire part Development of platform (GAS filter) Installation of cryogenic payload 31

32 4. Schedule Cooling test of cryostat Installation of Type A
Delivery of End sapphire mirrors Delivery of Front sapphire mirrors Installation of cryogenic payload 32 32 32

33

34 Extremely short commissioning
5. Schedule Official schedule iKAGRA observation : By end of 2015 bKAGRA installation and commissioning : By end of 2017 Current budget plan By March 2016 : One cryogenic payloads By March 2017 : Three cryogenic payloads (+ spare) By end of 2017 : Commissioning of bKAGRA Extremely short commissioning 34

35 35

36 3. Cryogenic payload Outline of cryostat Cryogenic payload Mirror
to SAS Cryogenic payload Cryostat Stainless steel t20mm Diameter 2.6m Height ~3.6m M ~ 10 ton Mirror View ports 4 Low vibration cryocooler unit Cryo-coolers Pulse tube, 60Hz 0.9 W at 4K (2nd) 36 W at 50K (1st) Main LASER beam Remote valve unit S. Koike


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