Cryogenic payloads and cooling systems (towards a third generation interferometer) part I: An Interferometer at Cryogenic Temperatures Piero Rapagnani I.N.F.N. Sezione di Roma Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Why cool the mirrors? Test masses and suspensions thermal noise reduces at low temperature: < x 2 T Thermoelastic noise both of the mirror substrates and coatings decrease: < x 2 aT 2 Thermal expansion rate a decreases at low temperature; Mechanical Q of some materials increases at low temperature @ w << w int T 2 < x Thermal lensing: Q Thermal conductivity increases and consequently reduces thermal gradients on the coating; Refraction index variation with temperature is very small at low temperature; Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 R&D on Cryogenics 1) Study of the refrigeration system - noise - refrigeration power 2) Suspension compatibility: thermal conduction and acoustic quality factor Q measurements 3) Sensors at low temperatures - accelerometers and position sensing devices - actuators Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Liquid helium Refrigerators Hybrid system Issues to cool the mirrors Refrigeration system: • The injected mechanical noise must be negligible, the sensitivity must be preserved: Good mechanical isolation between the mirror and the cooling system; • Cooling time of the mirror as low as possible: Good thermal couplings; High refrigeration power; Suspension system compatible with good mechanical and thermal couplings: • • Thermal conductivities change with temperature; Mechanical quality factor Q; Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Cryogenic fluids and G.W. Detectors The first cryogenic antenna in the world 1974-1980: M=20 kg, T =4 K , n ~ 5 kHz No excess noise Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 The second cryogenic antenna of the Rome group -1978: M~ 400 kg, T =4 K , n ~ 1.8 kHz Excess noise in the first phase of operation: Due to suspension system!! Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Advantage of the superfluid liquid Helium: the transition He phase transition to superfluid Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Data from the Antenna EXPLORER installed at CERN • The current technique to cool down a Resonant Antenna requires “Heavy Work” and several weeks • Detector duty cycle: less than 1 month. QuickTime™ and a TIFF (Uncompressed) decompressor are needed to see this picture. • For an interferometric antenna 6 masses to be cooled. • To preserve the duty cycle this “heavy work” must be done in parallel..... VIRGO Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 In a BIG Laboratory, large Cryogenic Facilities are possible The example of LHC at CERN: The Cryogenic Distribution Line (QRL) for the LHC (Large Hadron Collider). Each of the eight ~3.2 km QRL sectors is feeding Helium at different temperatures and pressures to the local cooling loops of the strings of superconducting magnets operating in superfluid helium below 2 K. With an overall length of 25.8 km the QRL has a very critical cost to performance ratio. QuickTime™ and a TIFF (LZW) decompressor are needed to see this picture. Technologies are available, but are VERY expensive and require extensive manpower Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 An alternative way to cool down without liquid helium: the new generation of Cryocoolers • A Pulse Tube Refrigerator (PTR) or "G-M style" pulse tube cryocooler, is a variant of a GiffordMcMahon (GM) cryocooler. First stage • PTR operate at low frequencies, typically <5 Hz. • Used a conventional oilflooded G-M compressor and a valve set near the cold head to convert the continuous flow of helium to a low frequency pressure wave. Piero Rapagnani – INFN Roma ILIAS Second stage Suitable for applications that require efficient operation: No moving parts in cold head. Minimal vibration, low acoustic noise, reliability. High efficiency: 2 to 3 times higher efficiency than GM cryocoolers for loads temperatures between 55 and 120 K. April 27th, 2006 A possible solution Passive vibrational isolation system for the heat link Long heat link Part of the refrigerating power absorbed by the isolators Attenuation of the refrigerating power Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Our solution Active vibration isolation system for the heat link Shorter heat link Refrigerating power preserved Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Q from refrigerator Vacuum Chamber and Cryostat Thermal Shields Marionetta Reaction Mass: Thermal Shield at ~ 4K High Efficiency Thermal Links Silicon Monolithic Wire Mirror Reaction Mass: Thermal Shield at ~ 4K Q from laser beam Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Q from refrigerator Vacuum Chamber and Cryostat Thermal Shields Marionetta Reaction Mass: Thermal Shield at ~ 4K High Efficiency Thermal Links Silicon Monolithic Wire Mirror Reaction Mass: Thermal Shield at ~ 4K Q from laser beam Rough Estimates give Tmirror ~ 10 K Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Q from Superfluid Helium Reservoir A hybrid system using Superfluid Helium could allow to reach T ~ 1.5 K Vacuum Chamber and Cryostat Thermal Shields Marionetta Reaction Mass: Thermal Shield at ~ 1.5 K High Efficiency Thermal Links Silicon Monolithic Wire Mirror Reaction Mass: Thermal Shield at ~ 1.5 K Q from laser beam Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 Thermal Links: Many Materials and Composites available Thermal behavior at low temperatures must be tested QuickTime™ and a TIFF (LZW) decompressor are needed to see this picture. Piero Rapagnani – INFN Roma ILIAS April 27th, 2006 The short/medium term future: The Cryogenic Suspension Test Facility Still non investigated Problems: Piezo Actuator Piezo Actuator Cryogenic (T~ 50 K) Suspension Elements Thermal link (T ~ 4 K) Piero Rapagnani – INFN Roma ILIAS April 27th, 2006