Cryopayload Suspension structure Kazuhiro Yamamoto Institute for Cosmic

Cryo-payload Suspension structure Kazuhiro Yamamoto Institute for Cosmic Ray Research (ICRR) the University of Tokyo KAGRA face to face meeting　　　 Institute for Cosmic Ray Research, The University of Tokyo, Kashiwa, Chiba, Japan 14 February 2014 1

Contribution R. Takahashi, K. Ono, T. Sekiguchi, Y. Sakakibara, C. Tokoku, M. Kamiizumi, U. Iwasaki, E. Hirose, A. Khalaidovski, R. Kumar, T. Uchiyama, S. Miyoki, M. Ohashi, K. Kuroda, T. Akutsu A, H. Ishizaki. A, F. E. Peña Arellano. A, T. Suzuki. B, N. Kimura. B, S. Koike. B, T. Kume. B, K. Tsubono. C, Y. Aso. C, T. Ushiba. C, K. Shibata. C, D. Chen. D, N. Ohmae. E, K. Somiya. F, R. De. Salvo. G, E. Majorana. H, L. Naticchioni. H, W. Johnson. I, A. Cumming. J, R. Douglas. J, K. Haughian. J, I. Martin. J, P. Murray. J, G. Hammond. J, S. Rowan. J , G. Hofmann. K, C. Schwarz. K, D. Heinert. K, R. Nawrodt. K, S. Goto. L, M. Tanaka. L, S. Ioka. M, K. Nakamoto. M, H. Nezuka. M, KAGRA collaboration ICRR. UT, NAOJA, KEKB, Phys. S. UTC, Astro. S. UTD, E. UTE, S. TITF, Sannio Univ. G, INFNH, Louisiana State Univ. I , University of Glasgow. J, Friedrich-Schiller-Universitaet Jena. K, Jecc Torisha. L, Toshiba Keihin Product Operations. M, KAGRA collaboration 2

0. Abstract Although there are many topics, here, I will explain (1)Schedule (2)Overall design (3)Monolithic sapphire suspension (4)Heat links 3

1. 2. 3. 4. 5. 6. 7. Contents Introduction Schedule Overall design Sapphire suspension Heat links ELi. TES activity Summary 4

1. Introduction Schematic view of KAGRA interferometer Four mirrors of arm cavity will be cooled. 3 k m 3 km Mozumi Y-end Sakonishi X-end Atotsu Center Kamioka mine (Underground site) Vibration isolation system, Cryocooler unit, Cryostat, Cryogenic payload 5

1. Introduction Outline of vibration isolation and cryostat 14 m 6

1. Introduction Outline of vibration isolation and cryostat 14 m Vibration Isolation Cryostat Cryogenic mirror 7

1. Introduction Outline of cryostat to SAS Cryogenic payload Cryostat Stainless steel t 20 mm Diameter 2. 6 m Height ~3. 6 m M ~ 10 ton Mirror View ports M Cryo-coolers Pulse tube, 60 Hz 0. 9 W at 4 K (2 nd) 36 W at 50 K (1 st) 4 Low vibration cryocooler unit ai n LA SE S. Koike R be a Remote valve unit m 8

Outline of vibration isolation and cryostat Heat link (pure Al) Pulse tube cryocoolers Sapphire fiber Sapphire mirror (About 20 K) Pulse tube cryocoolers 9

1. Introduction Schematic view of cryogenic payload Platform Intermediate Recoil Mass Intermediate Mass Test Mass (sapphire mirror) http: //gwdoc. icrr. u-tokyo. ac. jp/cgi-bin/private/Doc. DB/Show. Document? docid=210610

1. Introduction Outline of cryogenic payload Design is in progress. Details should be changed. Intermediate Recoil Mass Intermediate Mass Test Mass (sapphire mirror) Recoil Mass http: //gwdoc. icrr. u-tokyo. ac. jp/cgi-bin/private/Doc. DB/Show. Document? docid=210611

1. Introduction Outline of cryogenic payload in radiation shield http: //gwdoc. icrr. u-tokyo. ac. jp/cgi-bin/private/Doc. DB/Show. Document? docid=210612

1. Introduction “Sapphire monolithic suspension” One of the most important parts of KAGRA : Main sapphire mirrors are included. All parts are made from sapphire. Details should be changed. Mirror 13

2. Schedule “Official plan” End of 2017 : Cryogenic interferometer operation This is the significant milestone of KAGRA. Delivery of cryogenic payload By March 2015, One payload By March 2016, Three payloads For sapphire monolithic suspension, so aggressive ! The suspensions will be improved step by step. Initial phase suspension before final phase one is necessary. 14

2. Schedule “Initial phase” Larger thermal noise but more feasible First cryogenic payload (2014) is a “Initial phase”. R&D for final phase should be in progress at the same time. 　　Otherwise, thermal noise can not be reduced. We must do our best for three payloads as final phase (2015). 15

2. Schedule “Initial phase” Although thermal noise is large, it should be cooled (heat load test is necessary). It should be as simple as possible (budget and human resources). It can be replaced by final phase sapphire monolithic suspension later. 16

2. Schedule There are some ideas for “Initial phase” (1)No bonding, but screws, indium, cradle (2)Thick tungsten wires (they transfer heat) Any “Initial phase” plans have open issues. R&D must be finished by May 2014. Indium 17

3. Overall design Not sapphire suspension, but cryogenic payload in total Takanori Sekiguchi and Eiichi Hirose visited Stanford (December 2013) to discuss overall design with control system. Design and discussion are in progress. Preliminary design document http: //gwdoc. icrr. u-tokyo. ac. jp/cgi-bin/private/Doc. DB/Show. Document? docid=2106 18

3. Overall design E. Hirose organizes team to design the first cryogenic payload (Member : E. Hirose, T. Sekiguchi, R. Takahashi, R. Kumar). Dead line is June 2014. Short meeting every morning Some figures in 1. Introduction are brought by this team. 19

4. Sapphire suspension Sapphire monolithic suspension R&D for components are in progress. There a lot of items. Here, (1)Sapphire fiber (2)Sapphire blade spring (3)Sapphire bonding are introduced. 20

4. Sapphire suspension Sapphire fibers with nail heads are necessary to suspend mirrors. Test sample (T. Uchiyama) 21

4. Sapphire suspension Sapphire fibers with nail heads Mol. Tech Gmb. H (Germany) and IMPEX High. Tech Gmb. H (Germany) have already delivered ! Mol. Tech Gmb. H IMPEX High. Tech Gmb. H 22

4. Sapphire suspension Sapphire fibers with nail heads Quality check under collaboration with ET (ELi. TES) Q-value Measurement in Glasgow, Jena, Rome and Tokyo Thermal conductivity Measurement in Jena, Rome and Tokyo Strength Measurement in Glasgow 23

4. Sapphire suspension Sapphire fibers with nail heads Latest summary of Q and thermal conductivity Moltech IMPEX KAGRA requirement Q-value 107 at 20 K Thermal Conductivity 3000 at 20 K [W/m/K] 1*106 -6*106 5000 -6000 5000 IMPEX fibers satisfy the KAGRA requirement. 24

4. Sapphire suspension Sapphire fibers with nail heads Q of IMPEX fiber (D. Chen) Requirement : 5*106 https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 25

4. Sapphire suspension Sapphire fibers with nail heads Thermal conductivity of IMPEX fiber ar. Xiv: 1401. 2346 26

4. Sapphire suspension Sapphire fibers with nail heads Paper about thermal conductivity measurement was submitted to Classical and Quantum Gravity. ar. Xiv: 1401. 2346 27

4. Sapphire suspension Sapphire fibers with nail heads Strength test in Glasgow Fiber suspended weight. Moreover, weight was swung or pulled. Broken jointed end 15 kg test hang 28

4. Sapphire suspension Sapphire fibers with nail heads Strength test in Glasgow Fiber suspend weight. Moreover, weight was swung or pulled. G. Hammond reported in ELi. TES meeting (December 2013). https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 Safety factor derived from measurement : 3 - 16 Broken jointed end E. Majorana will visit Glasgow in this month and try strength test. 29

4. Sapphire suspension Sapphire fibers with nail heads Although we investigated fibers with round nail heads … Flat surfaces are necessary for bonding. New fibers with square nail head (IMPEX) is coming soon (end of February) ! Our plan for these fibers Surface flatness check (less than l/10 (l=630 nm)) Measurement of thermal conductivity and Q 30

4. Sapphire suspension Sapphire blade spring Sapphire fibers are thick (1. 6 mm in diameter) for heat transfer. Stretch by sapphire mirror weight (23 kg) : 21 mm If difference between length of 4 fibers are larger than 21 mm, there is no tension in one fiber ! Blade spring is necessary. 31

4. Sapphire suspension Sapphire blade spring (design is in progress) 46 mm R. Kumar 90 mm Vertical resonant frequency : 17. 4 Hz Max. stress : 159 MPa Bending breaking stress : 300 MPa (G. Hammond reported in ELi. TES meeting https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 ) 32

4. Sapphire suspension Bonding between sapphire fibers and sapphire mirror Hydroxide Catalysis Bonding (Ad. LIGO and Virgo) If fibers are broken, bonding parts must be taken apart … Candidates : Indium, Optical contact, Screws Test (in progress or near future plan) Strength test (tensile and shear) : KEK Thermal resistance : ICRR Mechanical dissipation : Jena and Glasgow (ELi. TES) 33

4. Sapphire suspension Bonding between sapphire fibers and sapphire mirror Hydroxide Catalysis Bonding Rebecca reported in ELi. TES meeting (Dec. 2013). https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 34

4. Sapphire suspension Bonding between sapphire fibers and sapphire mirror Hydroxide Catalysis Bonding (Rebecca Douglas[Glasgow], GWADW 2013). Strength (about 60 MPa) measured by her is 10 times larger than those of previous papers. T. Suzuki et al. , Journal of Physics; Conference Series 32(2006)309. A. Dari et al. , Classical and Quantum Gravity 27(2010)045010. Rebecca Douglas and Karen Haughian stayed in Japan in the last autumn. Rebecca reported in ELi. TES meeting (Dec. 2013). https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 35

4. Sapphire suspension Rebecca Douglas and Karen Haughian HCB Shear strength test (Strength vs crystal direction) ry a in m i l Pre https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 36

4. Sapphire suspension Next HCB shear strength test is in progress. https: //events. ego-gw. it/indico/conference. Other. Views. py? view=standard&conf. Id=7 37

4. Sapphire suspension Indium If fibers are broken, bonding parts must be taken apart … Indium is one of candidates. Hot welding Foil or evaporation (thickness: <20 mm) are prepared and heat is applied. When bonding parts are taken apart, heat and acid are applied. 38

4. Sapphire suspension We are preparing sample (KEK) … 39

4. Sapphire suspension We are preparing sample (KEK) … 40

4. Sapphire suspension We are preparing sample (KEK) … 41

4. Sapphire suspension We are preparing sample (KEK) … 42

4. Sapphire suspension We are preparing sample (KEK) … 43

4. Sapphire suspension R&D for integration of components One fiber prototype Full prototype 44

5. Heat links Outline of vibration isolation and cryostat Heat link (pure Al) Pulse tube cryocoolers 45

5. Heat links must be thick and short as heat path. However they must be thin and long as vibration path ! Dan Chen reports vibration via heat link in the next talk. Yusuke Sakakibara explains initial cooling time of cryogenic payload at the first talk in this afternoon. 46

6. ELi. TES activities ELi. TES: ET-LCGT interferometric Telescope Exchange of Scientists Grant for collaboration about cryogenic between KAGRA and ET European 7 th Framework Programme Marie Curie action (Mar. 2012 - Feb. 2016) European people can visit Japan for KAGRA. 47

6. ELi. TES activities A total of 25 visitors supported by ELi. TES in 2013 Note : Short stay for meeting is not counted. Germany (A total of 8 persons) Jena (A total of 6 persons), Hannover (2 persons) Netherlands NIKHEF (2 persons) United Kingdom Glasgow (3 persons) Italy (A total of 12 persons) Rome (3 persons), Sannio (A total of 9 persons) 48

6. ELi. TES activities ELi. TES in 2014 has already started ! Ettore Majorana (Rome) : Last week ! Discussion for cryogenic payload and vibration isolation Ronny Nawrodt and Stefanie Kroker (Jena) arrived this morning ! Cryogenic experiment 49

7. Summary Schedule is quite aggressive. We need initial phase suspension. Later it will be replaeced by final phase one. Design of initial phase suspension should be finished by next May. Overall design Discussion with Stanford Small team for design (short meeting every morning) Preliminary design document http: //gwdoc. icrr. u-tokyo. ac. jp/cgi-bin/private/Doc. DB/Show. Document? docid=2106 50

7. Summary Sapphire suspension Research and development for components (quality checks of fibers, design of blade spring, test for many kinds of bonding) are finished or in progress. New fibers with square nail heads will be delivered at the end of February. Heat link Dan Chen (vibration) and Yusuke Sakakibara (initial cooling time) report later. ELi. TES A total of 25 visitors in 2013. So far, 3 visitors in 2014. 51

Thank you for your attention ! 52

7. For future Some items for future research (not perfect list) (a)Investigation material properties (Q, thermal conductivity, strength etc. ) of coating, fiber and so on. (b)Sapphire bonding, Sapphire fiber clamp (c)Control and damping scheme Actuators and sensors at cryogenic temperature (d) Mechanical and thermal simulation for payload (e) Vertical spring in cryostat (f) Reduction of initial cooling time Thermal resistance of clamp. . (g) Baffles for scattered light in radiation shield (h) Assembly procedure 53

8. Summary Cryostat : Assembly is in progress. Cooling test is coming soon. Cryogenic duct : Optimum position of 5 buffles Future work : scattered light Cryocooler unit : Cooling test and vibration measurement : OK Cryogenic payload Preparation for 1/4 cryostat to check payload performance is in progress. Current main R&D topics Inital cooling time, Sapphire fiber with nail head, Coating mechanical loss, Vibration of shield 54

2. Issues (1)How to assemble Details of construction, clean room …. (2)Strength Tensile strength, development of clamp, sapphire bonding … (3)Control and damping system to reduce fluctuation and instability Actuators (what and where), resonant mode (frequency and Q) and so on 55

2. Issues (4)Cooling Temperature of mirror (below 20 K), initial cooling time, heat resistance of clamp … (5)Noise Thermal noise, vibration via vibration isolation system and heat links … 56

4. Sapphire fibers After Yusuke left …. Clamp for IMPEX fibers in Jena 57

4. Sapphire fibers Profile measurement in Glasgow 58

5. Sapphire suspension Sapphire fibers with nail heads Q measurement in Jena 59

Outline of vibration isolation and cryostat Vacuum Inner shield (8 K) Pulse tube cryocoolers Baffles Cryoduct chamber (300 K) Outer shield (80 K) 2 Pulse tube cryocoolers 60