Available online at ScienceDirect. Physics Procedia 67 (2015 ) Calibration of a HTS based LOX 400mm level sensor

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Available online at www.sciencedirect.com ScienceDirect Physics Procedia 67 (2015 ) 1169 1174 25th International Cryogenic Engineering Conference and the International Cryogenic Materials Conference in 2014, ICEC 25 ICMC 2014 Calibration of a HTS based LOX 400mm level sensor Karunanithi R. a, Jacob S. a, D. S. Nadig a, M.V.N. Prasad b, Abhay S. Gour a, Pankaj S. a, Gowthaman M. a, Sudharshan H. a a Centre for Cryogenic Technology, IISc Bangalore, India b Liquid Propulsion System Centre, ISRO, Bangalore, India Abstract The measurement of the cryogen level in a cryostage of space crafts is crucial. At the same time the weight of the sensor should be small as it affects the payload fraction of the space craft. An attempt to develop a HTS based level sensor of 400 mm for Liquid Oxygen (LOX) measurement was made. In the initial phase of testing, loss of superconductivity of HTS wire in LOX inside a cryostat was noticed. Thus, a new four wall cryostat was designed to have a stable LOX level to provide thermal stability to the HTS based LOX sensor. The calibration of the developed sensor was carried out against capacitance level sensor which was pre calibrated using diode array to verify its linearity and performance for different current excitation levels. The calibrations were carried out without heater wires. The automatic data logging was accomplished using a program developed in LabVIEW 11.0. c 2015 2014The Authors. Published by Elsevier by Elsevier B.V. B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/). Peer-review under responsibility of the organizing committee of ICEC 25-ICMC 2014. Peer-review under responsibility of the organizing committee of ICEC 25-ICMC 2014 Keywords: High temperature superconductor (HTS), Superconductivity, Superconductor quenching, Capacitance level sensor, Cryostat. 1. Introduction A HTS wire based liquid level sensor for LOX is discussed in this paper. A HTS wire based cryo-level sensor is compact, light-weight and is easy to fabricate. A Magnesium Boride (MgB 2 ) wire based liquid level sensor for Liquid Hydrogen (LH 2 ) has been developed by (Haberstroh and Zick (2006)). A similar attempt for the development of a HTS based level sensor for LOX and Liquid Nitrogen (LN 2 ) has been carried out (Karunanithi et al. (2014); Gour et al. (b)). The performance and repeatability of the developed sensor was found to be linear for liquid nitrogen when the calibration was carried out using PUF (Polyurethane foam) insulated cryostat, whereas the thermal stability issues were observed during the calibration when LOX calibration was attempted. This paper deals with the design of a four walled cryostat and the calibration results of a HTS based level sensor using LOX. The Four walled cryostat consists of a vacuum chamber, LN 2 guard chamber, second vacuum chamber and the calibration chamber. The cryostat is designed based on ASME Pressure vessel standards (Munn). The developed superconductor wire was calibrated against Karunanithi R. Tel.: +91-80-22933078; fax: +91-80-23601612. E-mail address: karun@ccf.iisc.ernet.in 1875-3892 2015 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/). Peer-review under responsibility of the organizing committee of ICEC 25-ICMC 2014 doi:10.1016/j.phpro.2015.06.182

1170 R. Karunanithi et al. / Physics Procedia 67 ( 2015 ) 1169 1174 (a) (b) (c) Fig. 1: Basic parts of cryostat (a) cylinder, (b) head and (c) lifting lug. a capacitance sensor which was calibrated using diode array (Gour et al. (a)). This paper discusses the cryostat design, physical mounting arrangements of the sensors, calibration procedure and results. The calibration details of the capacitance sensor using a diode array is discussed elsewhere [Gour et al. (a,b)] and automatic data logging and interfacing of the sensors are carried out using National Instrument Data Acquisition System and LabVIEW 11.0 software. Nomenclature D0 outer diameter [in] t sheet thickness [in] W Weld width [in] L inside crown radius [in] OR outside radius [in] Dia hole diameter [in] tkr inside kunckle radius [in] tb thickness before forming [in] 2. Cryostat design A four wall cryostat was built to provide thermal stability, by reducing the heat transfer to the inner most calibration vessel. The vessel has been designed in accordance with the ASME pressure vessel standards. The important parts of the vessel are: cylinder, head and lifting lugs as shown in Fig. 1. The following design procedure was adopted to fabricate the cryostat: Calculate the volume (D0,Length) required for mounting sensors and accessories as shown in Fig. 1(a) The maximum operating pressure for the vessel is 0.52 MPa. Determination of vessel wall thickness (t) which depends on operating pressure as shown in Fig. 1. Calculating the crown dimensions(d0,l,tkr,tb) to withstand designed pressure and the hanging load of the sensors as shown in Fig. 1(b). Design the lifting lugs that are very important for uniformly lifting the mounted sensors from the tank. The important design parameters for lugs are weld length (W), hook ID (Dia), hook thickness (OR) etc. as shown in Fig. 1(c).

R. Karunanithi et al. / Physics Procedia 67 ( 2015 ) 1169 1174 1171 Fig. 2: Schematic of 4-wall cryostat. Based on the above mentioned parameters carry out weld stress calculations to determine the strength of the weld to lift the mounted load To address the issue of loss of superconductivity when immersed in LOX and to provide better thermal stability to the filled cryogen in the inner most calibration vessel during calibration, high vacuum between the outer LN 2 jacket and the inner test chamber was created. Calculations were carried out to determine the order of vacuum to reduce conduction and convection based heat transfer. In order to avoid radiation heat transfer, the radiative heat load calculation was carried out, based on which the number of layers of the super insulation was estimated. The super insulation was wrapped in the vacuum chambers. After creating vacuum of the order of 10 3 Pa; getter material was fired to trap the hydrogen evolution and to improve the vacuum. Fig. 2 shows the schematic of the designed cryostat. The outer vacuum chamber contains 35 layers of superinsulation and the inner vacuum chamber has 8 layers. 3. HTS based 400 mm level sensor The level sensor consists of 12 strips of superpower 2G HTS SF12100 wire. Each strip is 420 mm long and the strips are soldered in a lapjoint fashion. Thus, the total length of the soldered stips is 5040 mm. The 240 mm of the total strip length was utilized for soldering the strips in lapjoint arrangement. Thus, 4800 mm of soldered strips is folded 12 times to get the active length of 400 mm. Each strip is electrically insulated using kapton tape and separated from each other using a spacer in between. A photograph of the HTS wire is shown in Fig. 3. The details of triple redundant capacitance level sensor (TRLS) has been discussed elsewhere (Gour et al. (b)).

1172 R. Karunanithi et al. / Physics Procedia 67 ( 2015 ) 1169 1174 (a) (b) Fig. 3: Photographs of (a) mounted sensors (HTS, TRLS Capacitance type and Diode Array) (b) experimental setup. (a) (b) Fig. 4: (a)schematic of DAQ interfacing system and (b) Graphical user interface LabVIEW Program Screenshot. 3.1. DAQ System Interfaced Using LAbVIEW Program The LabVIEW program was developed to read and log the instantaneous values of the voltages across the HTS wire, diode array and capacitance values from the capacitance type sensors via a capacitance bridge. The program is developed using LabVIEW 11 software. The schematic of interfacing of the DAQ used is shown in Fig. 3. The analog voltage of the HTS wire is measured using a high precision Keithely digital multimeter interfaced to the program via GPIB 488.2. The capacitance value is read through GPIB 488.2 using a capacitance bridge. The diode array was interfaced using NI-PXI-1033 which generates the digital output pulse to switch the diode using multiplexers and to measure the voltages across each set instantaneously. All the instantaneous values are logged into a text file. The plots of voltage and capacitance value with respect to time were plotted real time. The graphical user interface for the design program is shown in Fig. 4.

R. Karunanithi et al. / Physics Procedia 67 ( 2015 ) 1169 1174 1173 4. Calibration procedure Fig. 2 and 3, show the schematic and photograph of the calibration setup respectively. The calibration of the capacitance sensor against diode is discussed elsewhere [Gour et al. (b)]. The calibration procedure of HTS wire based level sensor against the TRLS capacitance sensor is as follows: 1. Mount the HTS sensor in line with capacitance type level sensor such that the zero position of the HTS based sensor is inside the active length of the capacitance level sensor. 2. Seal the top head of the vessel, fill the outer container with LN 2 till it is full and then start filling the inner container with cryogen. 3. The values of the capacitance level sensor are observed and recorded using the capacitance bridge. The inner container is gradually filled with cryogen at a constant rate till the capacitance readings reach a steady constant value. 4. Allow the setup to stablize for half an hour to attain thermal equilibrium. 5. Drain the liquid till the capacitance value becomes minimum. 6. Change the log file and restart the program for ascending calibration and fill the liquid gradually. 7. Ensure that the pressure inside the inner container is maintained at 0.2 bar. 8. Fill the liquid till the capacitance value reaches a stable maximum value. 5. Results and Discussions The calibration graphs of the HTS tape based level sensor against the capacitance type level sensor using LOX and LN 2 as cryogen are shown in Fig. 5(a) and (b) respectively. The ascending calibrations of HTS wire against the pre-calibrated capacitance type level sensor were carried out at constant flow rate of 1 lit/min while the pressure inside the inner vessel was maintained at 0.2 bar throughout the experiment. The changes in the capacitance and voltage values were recorded continuously for the full active length of the capacitance sensor. The experiment was repeated for different excitation current ratings i.e. 3A and 4A for LOX and 5A for LN 2. It has been observed that for different levels of LOX and LN 2, the voltage across the HTS wire is changed linearly. A straight line has been fit to the obtained curves to arrive at mathematical equations for further computations. 6. Conclusion The HTS based level sensor shows a linear response for LOX and LN 2 level change. The calibration was done for the complete measurement length of 400 mm. The weight of the sensor is less than 0.5 kg which is a major advantage. The behavior of the sensor was found to be stable for 3Aand4Aofconstant DC current for LOX and 5 A for LN 2. Acknowledgement The work was carried out as a development program with the financial support of ISRO Space Technology Cell (STC) and the authors wish to acknowledge support by ISRO STC to carry out the work. References Gour, A., Das, M., Karunanithi, R., Jacob, S., Prasad, M., Subramanian, D., a. Eleven point calibration of capacitance type cryo level sensors of lox and lh2 systems of cryogenic stage using four wire type discrete array level sensor setup. Proceeding of Twenty Third National Symposium on Cryogenics (NSC-23) Rourkela 2010. Gour, A., Karunanithi, R., Jacob, S., Prasad, M., Gowthaman, M., Deekshith, P., Raja, Rajan, R., b. High temperature superconductor based level sensor for liquid nitrogen. Proceeding of Twenty Fourth National Symposium on Cryogenics (NSC-24) Gandhinagar 2013. Haberstroh, C., Zick, G., 2006. A superconductive mgb2 level sensor for liquid hydrogen, in: Advances in Cryogenic Engineering: Transactions of the Cryogenic Engineering Conference-CEC, AIP Publishing. pp. 679 684.

1174 R. Karunanithi et al. / Physics Procedia 67 ( 2015 ) 1169 1174 Fig. 5: Calibration graph of HTS level sensor voltage versus TRLS Capacitance level sensor capacitance carried out at constant flow rate of 1l/min (a) LOX as a cryogen (b) LN 2 as cryogen. Karunanithi, R., Jacob, S., Nadig, D., Prasad, M., Gour, A., Gowthaman, M., Deekshith, P., Shrivastava, V., 2014. Design, development and calibration of hts wire based lox level sensor probe, in: Advances in cryogenic engineering: Transactions of the Cryogenic Engineering Conference-CEC, AIP Publishing. pp. 913 919. Munn, B.,. Asme code pressure vessel design. http://http://www.pveng.com/asme/asmeintro.php. Accessed: 2014-06-30.