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ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering#N#Conference - CEC, Vol. 53 | 2008

DEVELOPMENT OF CRYOGENIC LOOP HEAT PIPE

R. Karunanithi; S. Jacob; G.S.V.L. Narasimham; Ds Nadig; Upendra Behera; Dinesh Kumar

The design of a cryogenic loop heat pipe (CLHP) is presented in the paper. As the wick is required only in the evaporator section, very small pore size wicks can be used in applications with high thermal transport requirements and/or where the heat must be transported over a long distance against gravity. A FORTRAN program to solve the mathematical model and to determine the parameters for various boundary conditions has been developed. The CLHP is designed to transfer 5W heat at 70K using nitrogen or oxygen as working fluid. It will be a self priming type device which can operate against gravity with evaporator above the condenser as well as under microgravity condition. A G-M type single stage double inlet pulse tube refrigerator is coupled to the CLHP to test its performance. The mathematical model, design, fabrication integration of the heat pipe with the pulse tube system and testing with stainless steel wick at the evaporator will be described in the paper.


ADVANCES IN CRYOGENIC ENGEINEERING: Transactions of the Cryogenic Engineering Conference - CEC | 2004

Experimental Studies of Convection in a Single Stage Pulse Tube Refrigerator

S. Kasthurirengan; S. Jacob; R. Karunanithi; Upendra Behera; Ds Nadig

A single stage Pulse Tube Refrigerator has been designed, fabricated and operated with a 3kW GM type helium compressor with an indigenously developed rotary valve in the frequency range from 1.2 to 2.3Hz. The system produces a lowest temperature of 37.5K and a refrigeration power of 7.3W at 77K. The cold end temperature Tc of the Pulse Tube refrigerator depends on its orientation angle


ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC | 2014

Design, development and calibration of HTS wire based LOX level sensor probe

R. Karunanithi; S. Jacob; Ds Nadig; Mvn Prasad; Abhay Singh Singh Gour; M. Gowthaman; P. Deekshith; V. Shrivastava

\theta


ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC, Volume 57 | 2012

Performances of single and two-stage pulse tube cryocoolers under different vacuum levels with and without thermal radiation shields

S. Kasthurirengan; Upendra Behera; Ds Nadig; V. Krishnamoorthy

with respect to gravity vector and the increase in Tc arises due to the convection in the Pulse Tube. The lowest temperature occurs at


TRANSACTIONS OF THE CRYOGENIC ENGINEERING CONFERENCE—CEC: Advances in Cryogenic Engineering | 2010

PALLADIUM DOPED TIN OXIDE BASED HYDROGEN GAS SENSORS FOR SAFETY APPLICATIONS

S. Kasthurirengan; Upendra Behera; Ds Nadig

\theta = 0°


ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC, Volume 57 | 2012

Calibration and linearity verification of capacitance type cryo level indicators using cryogenically multiplexed diode array

R. Karunanithi; S. Jacob; Abhay Singh Singh Gour; M. Das; Ds Nadig; Mvn Prasad

. The increase in Tc with change in


Proceedings of the Twentieth International Cryogenic Engineering Conference (ICEC20) | 2005

Studies on a Single Stage GM type Pulse Tube Cryocooler Using an Indigenous Helium Compressor

S. Kasthurirengan; S. Jacob; R. Karunanithi; Upendra Behera; Ds Nadig; Anand N Bahuguni

\theta


Proceedings of the Twentieth International Cryogenic Engineering Conference (ICEC20) | 2005

Development and test of a cryopulverizer for reprocessing plastic wastes

S. Jacob; S. Kasthurirengan; R. Karunanithi; Upendra Behera; Ds Nadig

is small till about 70°. However, beyond this angle, Tc varies strongly and reaches a maximum value at


Review of Scientific Instruments | 2004

Development of a reliable and simple pressure wave generator for pulse tube refrigerators

R. Karunanithi; S. Jacob; S. Kasthurirengan; Upendra Behera; Ds Nadig

\theta ~ 120°


Cryogenics | 2010

Studies of cryotreatment on the performance of integral diaphragm pressure transducers for space application

Ds Nadig; S. Jacob; R. Karunanithi; R. Manjunatha; D Subramanian; Mvn Prasad; Geetha Sen; Abhay K. Jha

and decreases thereafter upto 180°.For a better understanding of convection phenomenon, detailed experimental studies have been performed on two pulse tubes with the same i.d. 13.3mm, but with lengths 250 and 300mm. The orientation dependence of Tc and the cooling power characteristics have been studied at different frequencies (1.2 Hz to 2.3 Hz) at two different pressures. The results have been analysed to obtain the experimentally observed heat flux due to convection,

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S. Jacob

Indian Institute of Science

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R. Karunanithi

Indian Institute of Science

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Upendra Behera

Indian Institute of Science

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S. Kasthurirengan

Indian Institute of Science

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Geetha Sen

Indian Space Research Organisation

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D Subramanian

Indian Space Research Organisation

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Mvn Prasad

Indian Space Research Organisation

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Dinesh Kumar

Indian Space Research Organisation

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R. Manjunatha

Indian Institute of Science

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