Demonstration of a Passive Loop Cooling Tower

Ojas Govardhan2, Chien-Hua Chen1, Josh Charles1, Sean Hoeing1, Mike Ellis1, and Richard Bonner1

1Advanced Cooling Technologies, Inc. Lancaster, PA

2CBRE, Seattle, WA

Abstract

Building HVAC consumes a significant amount of energy.  It is estimated that about 7% of the total electricity consumed by a water-cooled chiller is used to drive the condenser water pump.  A passive condenser loop is developed to curb this energy consumption by replacing the open pumped loop with a closed-loop thermosyphon system. The loop thermosyphon uses waste heat to circulate the condenser fluid, eliminating the electrical pumping power requirement and the large circulation pump.  Since it is a closed-loop, it also reduces the maintenance cost and enables both wet and dry cooling modes.  A demonstration unit with a riser about 40 feet (12.2 meters) tall is fabricated and tested at powers up to 25 kW.  The result has successfully shown that the loop thermosyphon is able to transfer the heat near isothermally (∆T < 0.4oC) over a long distance without the need for any pump and consuming any electricity. 

Keywords: Loop Thermosyphon, Evaporative Condenser, Passive Heat Transfer, Building HVAC

Nomenclature

HVAC       Heating, Ventilation, and Air Conditioning

DOE          Department of Energy

BTO          Building Technologies Office

            Liquid mass flow rate of refrigerant

V                  Vapor mass flow rate of refrigerant

DL              Liquid line diameter

DV             Vapor line diameter

ρL               Refrigerant liquid density

ρV               Refrigerant vapor density

EMI           Electromagnetic Interference

WBT         Wet Bulb Temperature

DBT          Dry Bulb Temperature

Roverall           Overall thermal resistance

measured      Measured mass flow rate

fg             Calculated mass flow rate (Heat of evaporation/input power)

Qin             Input power

hfg                    Heat of evaporation

1. INTRODUCTION

An open-loop evaporative cooling tower is commonly used in large buildings for heat rejection.  It requires a cooling water pump to circulate the cooling water from the chiller to the cooling tower.  This cooling water pump accounts for roughly 7% of the total cooling energy consumption [1].  The total electricity consumption from the water-cooled chiller (commercial building) is estimated at roughly 98B kWh in 2023 [2].  Based on these numbers, the cooling water pump accounts for 6.86B kWh/year with the cost of $686M/year (assuming $0.1/kWh).  This electricity consumption and the associated cost can potentially be saved by using a passive condenser loop, which consists of a loop thermosyphon and an evaporative condenser.

A loop thermosyphon uses heat to circulate working fluid between the heat source and the heat sink.  Waste heat from the chiller condenser vaporizes the working fluid, and the resultant density and pressure difference between the vapor line and liquid line provides a driving force to circulate the flow.  The vapor is condensed by an evaporative condenser, rejecting the ambient air through the force of air convection (dry mode) or evaporative cooling (wet mode).  The condensate backs to the heat source by gravity, and then the cycle repeats.  This mechanism enables a passive heat transfer over a very long distance (both vertically and horizontally).  Compared to the conventional thermosyphon, the loop thermosyphon separates the liquid return path from the vapor transport line, which eliminates the flooding limit and is able to use a more compact pipe size for large power transport.

Figure 1. Schematics of the passive condenser loop and the open-loop cooling tower. Note in the passive condenser loop, a small recirculating pump is still needed for spraying the cooling water to the condensing coil, but the electrical energy consumption is much smaller compared to the condenser water pump in the open-loop cooling tower.

Figure 1 shows the schematics of a passive condenser loop and a conventional open-loop cooling tower. The passive condenser loop uses a loop thermosyphon to transfer the heat via the latent heat of the refrigerant, while the open loop cooling tower uses an active pump to transfer the heat via the sensible heat of the cooling water.  The single-phase thermal resistance of the open-loop cooling tower in Figure 1 (Rsingle-phase loop) can be calculated via 1 / ṁCp.  On the other hand, the two-phase thermal resistance of the passive condenser loop (Rtwo-phase loop) can be calculated by the saturation temperature difference between the evaporator and condenser divided by the input power.  For refrigerants with steep saturation curves under the normal operating temperature, the saturation temperature difference of the loop thermosyphon can be very small (∆T < 1oC), compared to a typical pumped condensing water loop that has the ∆T around 5oC.  The reduced two-phase loop ∆T helps compensate for the less efficient in-direct evaporative cooling of the evaporative condenser.

The evaporative cooling consumes a large portion of the water supply (e.g. 28% of total water consumption in office buildings [3]).  The open-loop cooling tower cannot operate without water, while the closed passive condenser loop can operate in both wet and dry modes.  This feature reduces water consumption when the ambient temperature is low and increases building resilience during the water scarcity scenario.

In addition to energy and water saving, the closed-loop reduces the amount of regular maintenance as well as the chemical treatment compared to the conventional open-loop cooling tower, which provides additional cost savings.  The use of refrigerant as the working fluid also eliminates the freezing issue during the winter.

2. EXPERIMENTAL SETUP

A passive condenser loop was set up to demonstrate the feasibility of using a loop thermosyphon for the building HVAC application.  The system consists of four major components:

  1. Condenser – Evaporative Condenser
  2. Evaporator – Heat Exchanger
  3. Vapor Line
  4. Liquid Line

Figure 2 shows the schematic of the test loop.  Details of each component are described in the following subsections.

Figure 2. Schematic of the passive condenser loop test setup.

2.1 Condenser (Evaporative Condenser)

Since the loop thermosyphon is a closed system, a closed-loop condenser is needed.  A closed evaporative condenser is commercially available.  While the evaporative condenser is commonly integrated with a vapor compression system, it fits well to serve as the condenser for the loop thermosyphon.  The evaporative condenser includes several parallel serpentine coils where the vapor phase refrigerant is condensed to the liquid phase.  Due to the closed system, the heat rejection can be accomplished by either wet cooling (with water spray) or dry cooling (without water spray).  For wet cooling, a small water pump is needed to circulate the cooling water within the cooling tower. The evaporative condenser was placed on the rooftop of the building where ACT is located (Figure 3).  The rooftop is about 40 feet from the floor, where the evaporator heat exchanger is located.

Figure 3. An evaporative condenser integrated with the loop thermosyphon. The condenser is located on the rooftop of Burle business park where ACT is located.

The pressure drop inside the condenser is estimated via a two-phase, Friedel’s correlations.  The calculation shows that pressure drop is minimal (less than 1 Pa) for the operational range due to the very small mass flow rate and the large effective cross-section area.  The pressure drop caused by the condenser is insignificant compared to the pressure drop in the vapor and liquid lines.

2.2 Evaporator

A flat plate heat exchanger with four ports is used to serve as the evaporator.  Two ports are connected to the loop thermosyphon with working fluid (R134a) condensate entering from the bottom port and leaving from the top port. The other two ports are connected to a circulation hot water heater to serve as the heat load (Figure 2). The heat exchange is orientated in a countercurrent fashion, in which the hot water enters from the top port and leaves from the bottom port. The heater uses resistance coils to increase the temperature of the water and this hot water, connected by pipes to the evaporator inlet and outlet exchanges heat with the cool refrigerant in the loop. The input power (Qin) to the hot water can be adjusted by increasing the heater resistance and a maximum of 25 kW of heat can be inputted into the system. The water mass flow rate to the heat exchanger can be adjusted to control the outlet temperatures of the hot water (Q = ṁ × Cp × ΔT).  The working fluid pressure drop inside the evaporator is also calculated using Friedel’s correlations.  Due to the large size of the evaporator heat exchanger used in the setup, the calculated frictional pressure drop is also very small (2.3 Pa).

Figure 4. A flat plate heat exchanger is connected to the loop thermosyphon and a recirculation water heater.

2.3 Vapor Line

The vapor line carries the refrigerant in either single-phase vapor or two-phase mixture depending on the charge and input power.  To ensure the circular motion of the flow, and therefore the continuous heat rejection, the following equation (Equation 1) has to be satisfied:

∆Pliquid head = ∆Pvapor line + ∆Pliquid line + ∆Pevaporator + ∆Pcondenser (1)

Due to the high velocity in the gas phase, the ∆Pvapor line is likely dominant on the right-hand side of Equation 1.  For the single-phase (vapor) flow, the friction part of the ∆Pvapor line can be estimated via Darcy–the Weisbach equation.  In the current test setup design, it is assumed that the refrigerant exits the evaporator at the saturation conditions of 30°C and 770.1 kPa. The length of the vapor line is the combination of the vertical tubing (the height between the evaporator and the condenser, i.e. 40 feet) and the horizontal tubing (10 feet).  There is also a number of elbows that can cause minor losses.  The design of the vapor line pipe sizing is to balance the performance (pressure drop) and the cost.  The larger the pipe size, the lower the pressure drop, but also the higher the plumbing cost.  A 1.5” nominal diameter copper pipe was selected for the vapor line and the calculated frictional pressure drop is 2,332 Pa.

2.4 Liquid Line

The liquid line is the piped connection between the exit of the condenser to the evaporator. This downcomer line carries the refrigerant in a liquid state after the liquid changes its phase in the condenser. The liquid line is expected to carry the same mass flow rate of refrigerant as that of the vapor line. To evaluate the dimensions of the liquid line, the mass flow rate in the vapor line is equal to the mass flow rate in the liquid line.

For constant mass flow rate,

L = ṁV                                                                     (2)

̇Therefore,

DL = ((UV / UL) × (DV2 × ρV) / ρL)0.5            (3)

Since the vapor velocity is higher than the liquid velocity (UV / UL > 1), DL > ((DV2 × ρV) / ρV)0.5.

Considering

DV = 1.5” and densities at 30°C are ρL =1387.46 kg/m3 and ρV = 37.54 kg/m3

The minimum Diameter for the liquid line has to be > 0.25”.

Hence, from these calculations and considering the market availability, we choose the liquid line pipes to be 0.5” in diameter connecting the outlet of the condenser to the inlet of the evaporator.

Figure 5 Left shows the vapor and liquid lines.  Figure 5 Right shows the 3D drawing of the test setup with the aforementioned design inputs.

Figure 5. Left: Picture of the vapor and liquid lines outside the building.  Middle: 3D drawing of the test setup.  Right: Vapor and liquid lines inside the building.

2.5 Instrumentation and Total Volume

The entire testing loop needs to be monitored for pressures, temperatures, and flow rates to predict the performance of the loop. Four Resistance Temperature Detectors (RTDs) and Pressure Transducers (PTs) are used to monitor the temperature and the pressure at the evaporator outlet, condenser inlet, condenser outlet, and evaporator inlet.  A flow meter is installed on the liquid line section before the evaporator inlet to measure the liquid refrigerant flow rate in the system.  Three sight glasses on the liquid line at the height of 3 feet, 8 feet, and 13 feet in front of the ground are installed in order to check the height of the liquid column. Another sight glass is installed 3 feet below the condenser on the liquid line in order to check the quality of refrigerant at the exit of the condenser.  Two sight glasses are installed in the vapor line to visualize the quality of refrigerant leaving the evaporator.

The total volume of the loop was calculated to be 88.46 liters.  Figure 6 shows the system volume distribution of each component.

 

Figure 6. System volume distribution.

3. EXPERIMENTAL RESULTS

The passive condenser loop prototype was tested at multiple powers under different charges to evaluate the thermal performance. The system was charged initially to 60 lb (27.2 kg) of R-134a refrigerant. Then, 10 lb (4.54 kg) of charge was added to the system and the same tests were conducted at 70, 80, 90, 100, and 110 lb. charges. All the parameters including temperature, pressure, and refrigerant mass flow rate were measured for each charge. During the testing, the heater power was increased from 15 kW to 25 kW with a step of 2.5 kW.  Note that since the hot water circulation pump also generates heat, the measured powers (by circulation water calorimetry) were slightly higher than the heater input power as shown in Figures 8 to Figure 12.  A time interval of approximately 40 minutes between each test was allotted to ensure the system reaches the steady-state.

3.1 60 LB CHARGE

At the charge of 60 lb (Figure 7), the refrigerant occupied around 26% of the total loop volume. Figure 7 shows the temperature data of 60 lb charge under different input powers.  The condenser inlet temperature showed an early spike but the evaporator outlet maintained the same temperature as the rest of the loop suggesting the superheated vapor was caused by the vapor line wall conduction. As the heater power increases, the evaporator outlet temperature also showed a spike (at 20 kW) indicating the evaporator heat exchanger is drying out.  The system performance was hampered as the hot water out temperature increased significantly with the increased power.  The results indicated that the system was undercharge.

Figure 7. 60 lb charge test data.

3.2 70 LB CHARGE

By adding a 10 lb charge (70 lb, Figure 8), the system yields much better results than the previous test.  The heater temperature is around 45oC at 25 kW input power compared to > 60 oC for the 60 lb charge, even with a higher wet bulb temperature (WBT, 12.8oC vs. 3.3 oC). The hot water out temperatures maintains close to the loop liquid line temperatures (condenser outlet and evaporator inlet) throughout the tests.  While at the heater powers of 20-25 kW, the vapor line shows superheated vapor, it does not impact too much on the hot water out temperature as 60 lb charge does.  This suggests that no dry out happens in the evaporator heat exchanger and the superheated vapor in the vapor line is through vapor line wall conduction.

Figure 8. 70 lb charge test data.

3.3 80 LB CHARGE

At the charge of 80 lb (Figure 9), the volume occupied by the refrigerant equals 30.6 liters which accounts for 35% of the total loop thermosyphon volume. The heater water temperature is about 27oC initially and rises to 40oC at 25 kW power.  This lower heater temperature is contributed by the lower WBT.  At this charge, the vapor line and the liquid line temperatures are almost equal (isothermal loop behavior) throughout the test. The condenser inlet temperature is slightly lower than the evaporator outlet temperature indicating two-phase flow in the vapor line. The whole loop system maintains an isothermal two-phase flow as no superheated vapor or subcooled liquid is observed.

Figure 9. 80 lb charge test data.

3.4 90 LB CHARGE

At the charge to 90 lb (Figure 10), the loop behaves similar to 80 lb, except the slightly subcooled liquid is observed at higher powers as the condenser outlet temperature falls below the condenser inlet temperature.  This is because under this charge and the input powers, the liquid line is completely filled with liquid and the excess liquid refrigerant reaches inside the condenser leading to subcooling in the system.

Figure 10. 90 lb charge test data.

3.5 100 LB CHARGE

At a charge of 100 lb (Figure 11), prominent subcooling of 1~2oC is observed in the loop throughout the test. Some fluctuations in the heater power are observed due to electromagnetic interference (EMI). Under this charge, the flow in the vapor line is two-phase and the liquid line is completely filled with subcooled liquid.

Figure 11. 100 lb charge test data.

3.6 110 LB CHARGE

At the charge of 110 lb (Figure 12), the system is almost half (48%) volumetrically charged and a more significant subcooling of 3~4oC is seen in the liquid line.

Figure 12. 110 lb charge test data.

4. DISCUSSION

4.1 Loop Thermosyphon ∆T vs. Different Charges

The loop thermosyphon performance can be evaluated by the ΔT between the evaporator outlet and the condenser outlet (locations were shown in Figure 2).  Figure 13 shows the ΔT under 80 lb to 110 lb charges.  As can be seen, the increased charge increases the ΔT.  In addition, when the liquid head in the liquid line reaches the condenser (90 lb, 22.5kW), an increase in ΔT is observed due to subcooled condensate in the condenser outlet.

Figure 13. Loop thermosyphon ∆T vs. input power for different fluid charges.

4.2 Overall Thermal Resistance

The overall thermal performance is evaluated via the overall thermal resistance calculated via the following equation:

Roverall = (Heater Temperature – Wet Bulb Temperature) / Input Power  (4)

The input power is calculated from the calorimetry of the hot water loop.  Figure 15 shows the overall thermal resistance for different charges at 25 kW heater input.  At 60 lb charge, the evaporator has a significant dry out region at 25 kW power input, leading to high overall thermal resistance.  At 70 lb, while the evaporator outlet temperature shows superheated vapor in the vapor line, the thermal resistance is lower compared to other charges.  After 70 lb, further increasing charge shows a slight increase in the overall thermal resistance (Figure 14).

Figure 14. Left: Overall thermal resistance vs. fluid charge. Right: Wet-bulb temperature at different charge tests.

5. CONCLUSION

The feasibility of a passive condenser loop has been demonstrated for refrigerants with steep saturation curves under the normal operating temperature via a large-scale loop thermosyphon experiment.  The system was tested at six different fluid charges (R134a, from 60 lb to 110 lb at a 10 lb increment) and at 5 different powers (15 kW to 25 kW at a 2.5 kW increment).  The results validate the loop is able to deliver a large power (25 kW) over a long distance (40 feet vertical + 10 feet horizontal) with a minimum ΔT (< 0.4oC).

At 60 lb charge, dry out in the evaporator was observed resulting in a large overall thermal resistance.  When the charge increases to 70 lb, no dry out in the evaporator as the overall resistance becomes minimal (Figure 14).  However, an increased vapor line temperature was observed at 22.5 kW due to superheated vapor (Figure 8).  When the charge increases to 80 lb, the superheated vapor is eliminated, but the overall resistance slightly higher than the 70 lb.  When the charge increases to 90 lb, the ΔT of the loop thermosyphon increases at higher power (22.5 kW, Figure 13) due to the liquid head reaching the condenser and therefore subcooled liquid.  The ΔT increases with higher charges (100 lb and 110 lb) and higher input powers since more liquid is pushed into the condenser and therefore more subcooling. The overall thermal performance of the current setup however was observed less dependent on different charges due to the much larger thermal resistances of the evaporator (between the recirculating hot water and the loop thermosyphon) and the condenser (between the evaporative condenser and the ambient).

ACKNOWLEDGEMENTS

This work is supported by the Department of Energy National Energy Technology Laboratory (NETL) under the contract number DE-FE0031657.  Ms. Barbara Conery is the program manager.  The authors thank Mr. Phil Martin, Mr. Dennis Winters, Mr. Jeff Polignone, and Mr. John Brubaker at Advanced Cooling Technologies, Inc. for setting up the test loop and helping perform the experiments.

REFERENCES

[1] Frank Morrison, “Saving Energy with Cooling Towers,” ASHRAE Journal, February 2014

[2] https://scout.energy.gov/baseline-energy-calculator.html

[3] https://www.epa.gov/sites/production/files/2017-01/documents/ws-commercial-factsheet-offices.pdf

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Josh Charles and Nathan Van Velson, 5-6th Thermal and Fluids Engineering Conference (TFEC), pages 239-248. (video presentation included).

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Interfacial thermal resistance between nm-thick MoS2 and quartz substrate:  A critical revisit under phonon mode-wide thermal non-equilibrium.

Hamidreza Zobeiria, Nicholas Hunter, Nathan Van Velson, Cheng Deng, Qianying Zhang, Xinwei Wang, Nano Energy, V.89, Part A, November 2021, 106364.

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Development of Solid-State Waste Heat Delivery System for Electric Aircraft

Heat pipe-based thermal delivery system to efficiently manage the waste heat of an electric aircraft.

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Hot Reservoir Variable Conductance Heat Pipe with Advanced Fluid Management

Advanced Cooling Technologies, Inc. (ACT) in collaboration with Case Western Reserve University (CWRU) is developing a reliable VCHP configuration under the NASA STTR program. Presented at: 50th International Conference on Environmental Systems ICES-2021-242, 12-15 July 2021

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Thermal Management System for Lunar Ice Miners

Presented at: 50th International Conference on Environmental Systems ICES-2021-235, 12-15 July 2021

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ADVANCED WASTE HEAT RECOVERY TECHNOLOGY BY THERMO-RADIATIVE CELL FOR NUCLEAR SPACE POWER APPLICATIONS

In order to satisfy the long-lasting and high energy/power density requirements for NASA deep space exploration missions, Pu-238 has been identified as one of the most suitable radioisotope fuels for GPHS modules since the 1960s. Knoxville, TN, April 6 – April 9, 2020, available online at https://nets2020.ornl.gov

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Development of a Passive Thermal Control Valve for 3D-Printed Loop Heat Pipes

The focus of this work is the development of a passive thermal control valve (TCV) integrated with the design of a 3D-Printed LHP evaporator. (ICES) 2021, Virtual, July 12-15, 2021.

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Development of a Cold Plate for Spatial and Temporal Temperature Uniformity

Development of a cold plate which, through variable thermal conductance, provides spatial and temporal temperature uniformity to address this need. (ICES) 2021, Virtual, July 12-15, 2021.

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A Variable-View-Factor Two-Phase Radiator Manufactured Via Ultrasonic Welding

ACT in collaboration with Edison Welding Institute is developing a manufacturing process for the VVFTPR. This paper describes the ultrasonic welding technique chosen for manufacturing as well as material choices and other considerations. In collaboration with Edison Welding Institute, Columbus, Ohio. (ICES) 2021, Virtual, July 12-15, 2021

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Pumped 2-Phase Cooling as an Enabler for a Modular, Medium- Voltage, Solid-State Circuit Breaker

In collaboration with Eaton Research Labs, USA, ACT's Andy Slippey and Devin Pellicone presented Pumped Two-Phase Cooling as an enable for Modular, Medium Voltage, Solid-State Circuit Breaker. PCIM Europe digital days 2021, 3 – 7 May 2021 I http://www.pcim-europe.com/

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THERMALLY-DRIVEN EJECTOR FOR VACUUM FREEZING DESALINATION AT THE TRIPLE POINT

Jianjian Wang, Fangyu Cao, "Thermally-Driven Ejector for Vacuum Freezing Desalination at the Triple Point," 5th Thermal and Fluids Engineering Conference (TFEC), 2020-32060.

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Computational Fluid Dynamics Model for a Variable Conductance Thermosyphon

Cho-Ning Huang, Kuan-Lin Lee, Calin Tarau, Yasuhiro Kamotani and Chirag R. Kharangate, "Computational Fluid Dynamics Model for a Variable Conductance Thermosyphon", Case Studies in Thermal Engineering, vol 25, 2021.

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Technoeconomic Benefits of Film-Forming Amine Products Applied to Steam Surface Condensers

Sean H. Hoenig, et al., PPCHEM Journal-23 2021/01, pp. 4-16.

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Surface-Functionalized Boron Nanoparticles with Reduced Oxide Content by Nonthermal Plasma Processing for Nanoenergetic Applications

Prawal P. K. Agarwal, Devon Jensen, Chien-Hua Chen, Robert M. Rioux, and Themis Matsoukas; ACS Applied Materials & Interfaces Article ASAP, DOI: 10.1021/acsami.0c20825

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Development of Variable-View-Factor and Deployable Two-Phase Radiator

Jeff Diebold, Calin Tarau, Andrew Lutz and Srujan Rokkam, “Development of Variable-View-Factor and Deployable Two-Phase Radiator", ICES 2020-317

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Modeling of a Loop Thermosyphon Supplying Solar Energy to a Desalination Boiler

Josh Charles et al., SolarPaces, September 29, 2020, https://2020.solarpaces-conference.org/home.html

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Turbulent flow and heat flux analysis from validated large eddy simulations of flow past a heated cylinder in the near wake region

Arpan Sircar, Mark Kimber, Srujan Rokkam, and Gerrit Botha, Physics of Fluids 32, 125119 (2020)

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Plasma-Assisted Dry Methane Reforming for Syngas Production

Howard Pearlman et al., Spring Technical Meeting of the Eastern States Section of the Combustion Institute, March 8-11, 2018.

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Direct Simulations of Biphilic-Surface Condensation: Optimized Size Effects

Zijie Chen, Sanat Modak, Massoud Kaviany, Richard Bonner, “Direct Simulations of Biphilic-Surface Condensation: Optimized Size Effects” Frontiers in Heat and Mass Transfer (FHMT), vol 14, 2020/2/27

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Cooling High Power Processing Devices Onboard Satellites: Testing Considerations for Space Copper-Water Heat Pipes (SCWHPs)

Pete Dussinger, Jens Weyant, Ryan Spangler. Advanced Cooling Technologies, Inc., (Lancaster, PA).

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Rigorous prediction of Raman intensity from multi-layer films

Nathan Van Velson, Hamidreza Zobeiri, and Xinwei Wang Optics Express Vol. 28, Issue 23, pp. 35272-35283 (2020)

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Development of High Heat Flux Titanium-Water CCHPs

Andrew Lutz et al., International Conference on Environmental Systems, ICES-2020-323. (2020)

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Advanced Hot Reservoir Variable Conductance Heat Pipes for Planetary Landers

Kuan-Lin Lee et al. , International Conference on Environmental Systems, ICES-2020-579. (2020)

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Thermal Concept for Planetary Ice Melting Probe

Kuan-LinLee et al., International Conference on Environmental Systems, ICES-2020-201. (2020)

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Role of substrate thermal conductivity and vapor pressure in dropwise condensation

Sean H. Hoenig et al., Applied Thermal Engineering, Vol. 178, September 2020, 115529

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Innovative Solutions to Meet Thermal Performance of High-Power Laser Systems

Bryan Muzyka, SPIE Photonics West, San Francisco, CA, February 1-6, 2020.

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Titanium-Water Heat Pipe Radiators for Space Fission Power System Thermal Management

Lee, K., Tarau, C., Anderson, W.G. et al., Microgravity Science Technology. (2020)

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Thin hybrid capillary two-phase cooling system

Mohammad Reza Shaeri, et al., International Communications in Heat and Mass Transfer, 112, March 2020, 104490

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Vertical Surface Dropwise Condensation Heat Transfer Using Self-Healing Coatings

Sean H. Hoenig et al., 19th IAHR International Conference on Cooling Towers and Heat Exchangers , Washington, DC, October 8-10 2019

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Thermoradiative Cell – A New Waste Heat Recovery Technology for Space Power Applications

Jianjian Wang et al., International Energy Conversion Engineering Conference, Indianapolis, IN, August 19-22 2019

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A Systems Study of a Stirling Convertor based Space Nuclear Power System

Joesph VanderVeer et al., International Energy Conversion Engineering Conference, Indianapolis, IN, August 19-22 2019

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Prototype Results for a Salt Hydrate PCM Thermal Energy Storage System

Sean Hoenig et al., ASME 2019 Summer Heat Transfer Conference (HT2019), Bellevue, WA, July 15-18 2019

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Variable-View-Factor Two-Phase Radiator

Andrew Lutz et al., 49th International Conference on Environmental Systems (ICES), Boston, Massachusetts, July 7-11 2019

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Development of a 3D Printed Loop Heat Pipe

Bradley Richard et al., 49th International Conference on Environmental Systems (ICES), Boston, Massachusetts, July 7-11 2019

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24 Hour Consumable-based Cooling System for Venus Lander

Kuan-Lin Lee and Calin Tarau, 49th International Conference on Environmental Systems (ICES), Boston, Massachusetts, July 7-11 2019

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Thermal Control of Lunar and Mars Rovers/Landers Using Hybrid Heat Pipes

Mohammed T. Ababneh et al, Journal of Thermophysics and Heat Transfer, Vol. 33(3), July 2019

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3D Printed Thermal Management System for the Next Generation of Gallium Nitride-Based Solid State Power Amplifiers

Mohammed T. Ababneh et al., 49th International Conference on Environmental Systems (ICES), Boston, Massachusetts, July 7-11 2019

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Performance Evaluation of a Loop Thermosyphon Based Heat-Sink for High Power SiC-based Converter Applications

Sayan Acharya, et al., IEEE: Transactions on Components, Packaging and Manufacturing Technology, June 17 2019, 1-1

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Development of a 3D Printed Loop Heat Pipe

Bradley Richard, et al., Semi-Therm, San Jose, CA, March 18 – 22 2019

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Enhanced vacuum freezing for thermal desalination at the triple point

Fangyu Cao and Jianjian Wang, 4th Thermal & Fluids Engineering Conference, Las Vegas, NV, April 14-17 2019

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Advances in Lightweight Heat Sinks

Mohammad Reza Shaeri and Richard Bonner, 4th Thermal & Fluids Engineering Conference, Las Vegas, NV, April 14-17 2019

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A Nonlocal Peridynamics Modeling Approach for Corrosion Damage and Crack Propagation

Srujan Rokkam, et al., Theoretical and Applied Fracture Mechanics, 101, 2019, 373–387 (2019)

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Vortex dynamics and heat transfer of longitudinal vortex generators in a rectangular channel

Zhaoqing Ke, et al., International Journal of Heat and Mass Transfer, 132, 875-885 (2019)

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Meshless Peridynamics Method for Modeling Corrosion Crack Propagation

Srujan Rokkam, et al., 6th International Crack Paths Conference, Verona, Italy, September 19-21 2018

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Bio-inspired self-agitator for convective heat transfer enhancement

Zheng Li et al., Applied Physical Letters 113, 113703 (2018)

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Corrosion testing of metals in contact with calcium chloride hexahydrate used for thermal energy storage

S. J. Ren et al., Materials and Corrosion, Volume 68, Issue 10, July 2017

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Thermal energy storage with tunable melting point phase change materials

Fangyu Cao et al., Proceedings of the 16th International Heat Transfer Conference, Bejing, China, August 10-15, 2018

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Loop Heat Pipe Wick Fabrication via Additive Manufacturing

Bradley Richard et al., 48th International Conference on Environmental Systems, Albuquerque, New Mexico, July 8-12, 2018

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Design Analysis and Performance testing of a Novel Passive Thermal Management System for Future Exploration Missions

Angel R. Alvarez-Hernandez et al., International Conference on Environmental Systems, Albuquerque, NM July 8-12, 2018

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High-Heat-Flux (> 50 W/cm2) Hybrid Constant Conductance Heat Pipes

Mohammed T. Ababneh et al. International Conference on Environmental Systems, Albuquerque, NM, July 8-12, 2018

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Demonstration of Copper-Water Heat Pipes Embedded in High Conductivity (HiK™) Plates in the Advanced Passive Thermal eXperiment (APTx) on the International Space Station (ISS)

Mohammed T. Ababneh et al., International Conference on Environmental Systems, Albuquerque, NM July 8-12, 2018

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Advanced Passive Thermal eXperiment (APTx) for Warm-Reservoir Hybrid-Wick Variable Conductance Heat Pipes on the International Space Station (ISS),”

Calin Tarau, et al., International Conference on Environmental Systems (ICES 2018), Albuquerque, NM July 8-12, 2018

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Apparatus for Characterizing Hot Surface Ignition of Aviation Fuels

Andrew Slippey et al., AIAA Propulsion and Energy Forum, (AIAA 2018-4708), Cincinnati, OH, July 9-12, 2018

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Titanium Water Heat Pipe Radiators for Space Fission System Thermal Management

Kuan-Lin Lee, et al., 19th International Heat Pipe Conference, Pisa, Italy, June 10-14, 2018

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Copper-Water and Hybrid Aluminum-Ammonia Heat Pipes for Spacecraft Thermal Control Applications

Mohammed Ababneh, et al., 19th International Heat Pipe Conference, Pisa, Italy, June 10-14, 2018

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Loop Heat Pipe Wick Fabrication via Additive Manufacturing

Bradley Richard, et al., 19th International Heat Pipe Conference, Pisa, Italy, June 10-14, 2018

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Meshless Computational tools for Fatigue Damage and Failure Modeling

Srujan Rokkam et al., ITHERM 2018 (17th Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems), San Diego, CA, May 29 – June 1

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Thermal Management Technologies for Embedded Cooling Applications

Andy Slippey et al., ITHERM 2018 (17th Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems), San Diego, CA, May 29 – June 1

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Experimental Investigation of Gravity-Driven Two-Phase Cooling for Power Electronics Applications

Devin Pellicone, PCIM 2018, Nuremberg, Germany, June 5-7, 2018.

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Experimental, Numerical and Analytic Study of Unconstrained Melting in a Vertical Cylinder with a Focus on Mushy Region Effects

Chunjian Pan,⇑, Joshua Charles, Natasha Vermaak, Carlos Romero, Sudhakar Neti, Energy Research Center, Lehigh University, Bethlehem, PA 18015, USA Ying Zheng, Chien-Hua Chen, Richard Bonner III, Advanced Cooling Technologies, Inc., Lancaster, PA 17601, USA International Journal of Heat and Mass Transfer, Accepted 2 April 2018

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A Non-Thermal Gliding Arc Plasma Reformer for Syngas Production

Howard Pearlman, 3rd Thermal and Fluids Engineering Conference (TFEC), Fort Lauderdale, FL, March 4-7, 2018

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An Innovative Volatile Organic Compound Incinerator

Joel Crawmer et al., International Thermal Treatment Technologies (IT3), Houston, TX, March 6-8 2018

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Developing High-Temperature Water-Repellent Glass Fibers Through Atomic Layer Deposition

Mohammad Reza Shaeri et al., 3rd Thermal and Fluids Engineering Conference (TFEC), Fort Lauderdale, FL, March 4-7, 2018.

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Dropwise Condensation on Hydrophobic Microporous Powder and the Transition to Intrapowder Droplet Removal

Sean Hoenig and Richard W. Bonner, III, 3rd Thermal and Fluids Engineering Conference (TFEC), Fort Lauderdale, FL, March 4-7, 2018.

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The Key Role of Pumping Power in Active Cooling Systems

Mohammed Reza Shaeri, 3rd Thermal and Fluids Engineering Conference (TFEC), Fort Lauderdale, FL, March 4-7, 2018.

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Nucleating agent enhanced thermal desalination at the triple point

Fangyu Cao et al., 3rd Thermal and Fluids Engineering Conference (TFEC), Fort Lauderdale, FL, March 4-7, 2018

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Titanium Water Heat Pipes for Space Fission Power Cooling

Kuan-Lin Lee et al. ANS NETS 2018 – Nuclear and Emerging Technologies for Space Las Vegas, NV, February 26 – March 1, 2018

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Dropwise Condensation on Superhydrophobic Microporous Wick Structures

Sean Hoenig, Richard Bonner, Ph.D., ASME doi:10.1115/1.4038854 History: Received April 28, 2017; Revised December 06, 2017

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A Peridynamics-FEM Approach for Crack Path Prediction in Fiber-Reinforced Composites

Srujan Rokkam et al., 2018 AIAA SciTech Forum, Kissimmee, FL, January 8-12, 2018.

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Vapor chambers with hydrophobic and biphilic evaporators in moderate to high heat flux applications

Mohammad Reza Shaeri, Daniel Attinger, Richard W. Bonner III, Applied Thermal Engineering, Volume 130(5), Pages 83-92, February 2018

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Model-Based Dynamic Control of Active Thermal Management System

ASME 2017 International Mechanical Engineering Congress and Exposition IMECE 2017 - 71918, November 3-9, 2017 Tampa, FL. Nathan Van Velson, Srujan Rokkam, Quang Truong, Bryan Rasmussen

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Efficient optimization of a longitudinal finned heat pipe structure for a latent thermal energy storage system

Sean Hoenig et al., Energy Conversion and Management, 153, pp. 93-105, 2017.

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The Electroneutrality Constraint in Nonlocal Models

Eitan Lees, Srujan Rokkam, Sachin Shanbhag, and Max Gunzburger. Journal of Chemical Physics 147, 124102 (2017)

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Heat Pipe Embedded Thermoelectric Generator for Diesel Generator Set Waste Heat Recovery

James Schmidt and Mohammed Ababneh. 14th International Energy Conversion Engineering Conference, AIAA Propulsion and Energy Forum, (AIAA 2016-4605)

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Efficient Modeling of Phase Change Material Solidification with Multidimensional Fins

C. Pan et al., International Journal of Heat and Mass Transfer, Vol. 115, Part A, pp. 897-909, December 2017.

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Integrated Vapor Chamber Heat Spreader for Power Module Applications

Clayton Hose et al., InterPACK 2017, San Francisco, CA, August 29 – September 1, 2017

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Heat transfer and pressure drop in laterally perforated-finned heat sinks across different flow regimes

Mohammad Reza Shaeri, Richard Bonner Advanced Cooling Technologies, Inc., Lancaster, PA 17601, United States , Available online 24 August 2017

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Feasibility Study of a Vapor Chamber with a Hydrophobic Evaporator Substrate in High Heat Flux Applications

Mohammad Reza Shaeria et al., International Communications in Heat and Mass Transfer, Vol. 86, pp. 199–205, 2017.

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Effect of Perforation Size to Perforation Spacing on Heat Transfer in Laterally Perforated-Finned Heat Sinks

Mohammed Reza Shaeri, and Richard W. Bonner III, ASME 2017 Summer Heat Transfer Conference (HT2017), July 9-14, 2017, Bellevue, Washington, USA

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Two-Phase Heat Exchanger with Thermal Storage Capability for Space Thermal Control System

Two-Phase Heat Exchanger with Thermal Storage Capability for Space Thermal Control System, Kuan-Lin Lee, et al. 47th International Conference on Environmental Systems (ICES 2017), July 16-20, 2017, Charleston, South Carolina

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Advanced Passive Thermal Experiment for Hybrid Variable Conductance Heat Pipes and HiK™ Plates on the International Space Station

Advanced Passive Thermal Experiment for Hybrid Variable Conductance Heat Pipes and HiK™ Plates on the International Space Station, Mohammed T. Ababneh, et al. 47th International Conference on Environmental Systems (ICES 2017), July 16-20, 2017, Charleston, South Carolina

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LHP Wick Fabrication via Additive Manufacturing

LHP Wick Fabrication via Additive Manufacturing. Bradley Richard, et al. 47th International Conference on Environmental Systems (ICES 2017), July 16-20, 2017, Charleston, South Carolina

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High Temperature Water Heat Pipes for Kilopower System

Derek Beard et al., IECEC – AIAA Propulsion and Energy Forum and Exposition (AIAA Propulsion and Energy 2017), July 10-12, Atlanta, Georgia

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Sodium Heat Pipes for Space and Surface Fission Power

Derek Beard, Calin Tarau, and William G. Anderson, IECEC – AIAA Propulsion and Energy Forum and Exposition (AIAA Propulsion and Energy 2017), July 10-12, Atlanta, Georgia

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Laminar Forced Convection Heat Transfer From Laterally Perforated-Finned Heat Sinks

Mohammad Reza Shaeri and Richard W. Bonner III, Applied Thermal Engineering, Volume 116, pp. 406-418, April 2017.

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An Innovative Volatile Organic Compound Incinerator

Joel Crawmer et al., 10th U. S. National Combustion Meeting, College Park, MD, April 23-26, 2017

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A Swiss Roll Style Combustion Reactor for Non-Catalytic Reforming

Ryan Zelinsky et al., 10th U. S. National Combustion Meeting, College Park, MD, April 23-26, 2017

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Thermal Resistance Network Model for Heat Pipe-PCM Based Cool Storage System

Sean Hoenig et al., 2nd Thermal and Fluid Engineering Conference (TFEC2017), Las Vegas, NV, April 2-5 2017.

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Development of Low Cost Radiator for Surface Fission Power

Calin Tarau et al., International Energy Conversion Engineering Conference (IECEC), Salt Lake City, UT, July 25-27, 2016

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Generation of amorphous carbon models using liquid quench method: A reactive molecular dynamics study.

Raghavan Ranganathan, Srujan Rokkam, Tapan Desai, Pawel Keblinski Carbon, Volume 113, March 2017, Pages 87–99

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Self-Venting Arterial Heat Pipes for Spacecraft Applications

Derek Beard, William G. Anderson, and Calin Tarau, International Energy Conversion Engineering Conference (IECEC), Salt Lake City, UT, July 25-27, 2016

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Hybrid Heat Pipes for Lunar and Martian Surface and High Heat Flux Space Applications

Mohammed T. Ababneh et al., International Conference on Environmental Systems (ICES) 2016, Vienna. Austria, July 11-14, 2016

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Development of a Pumped Two-phase System for Spacecraft Thermal Control

Michael C. Ellis and Richard C. Kurwitz, International Conference on Environmental Systems (ICES) 2016, Vienna. Austria, July 11-14, 2016

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Vapor Chamber with Phase Change Material-Based Wick Structure

James Yun, Calin Tarau, and Nathan Van Velson, International Conference on Environmental Systems (ICES) 2016, Vienna. Austria, July 11-14, 2016

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A Novel Closed System, Pressure Controlled Heat Pipe Design for High Stability Isothermal Furnace Liner Applications

Taylor Maxwell et al., 13th International Symposium on Temperature and Thermal Measurements in Industry and Science (TEMPMEKO 2016), Zakopane, Poland, June 26 – July 1, 2016

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Thermal Enhancements for Separable Thermal Mechanical Interfaces

James Schmidt et al., AIAA Thermophysics Conference, Washington, D.C., June 13-17, 2016

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The Design of a Split Loop Thermosyphon Heat Exchanger for Use in HVAC Applications

Daniel Reist et al., Joint 18th International Heat Pipe Conference and 12th International Heat Pipe Symposium, Jeju, Korea, June 12-16, 2016

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Hot Reservoir Stainless-Methanol Variable Conductance Heat Pipes for Constant Evaporator Temperature in Varying Ambient Conditions

Jens Weyant et al., Joint 18th International Heat Pipe Conference and 12th International Heat Pipe Symposium, Jeju, Korea, June 12-16, 2016

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Hybrid Variable and Constant Conductance Heat Pipes for Lunar and Martian Environments and High Heat Flux Space Applications

Mohammed T. Ababneh et al., Joint 18th International Heat Pipe Conference and 12th International Heat Pipe Symposium, Jeju, Korea, June 12-16, 2016

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Self-Venting Arterial Heat Pipes for Spacecraft Applications

William G. Anderson et al., Joint 18th International Heat Pipe Conference and 12th International Heat Pipe Symposium, Jeju, Korea, June 12-16, 2016

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Performance Life Testing of a Nanoscale Coating for Erosion and Corrosion Protection in Copper Microchannel Coolers

Nathan Van Velson and Matt Flannery, IEEE ITherm Conference, May 31-June 3, 2016, Las Vegas, NV

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Heat Pipes used as Heat Flux Transformers and for Remote Heat Rejection

Devin Pellicone and Jens Weyant, PCIM Europe 2016, Nuremberg, Germany, May 10-12, 2016

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Enhanced Filmwise Condensation with Thin Porous Coating

Ying Zheng, Chien-Hua Chen, Howard Pearlman, Richard Bonner, First Pacific Rim Thermal Engineering Conference, PRTEC, March 13-17, 2016, Hawaii's Big Island, USA.

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Optimized Alkali Metal Backup Cooling System Tested with a Stirling Convertor

Calin Tarau, Nuclear and Emerging Technologies for Space (NETS) 2016, Huntsville, AL, February 22-25, 2016.

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Status of the Development of Low Cost Radiator for Surface Fission Power II

Calin Tarau, Nuclear and Emerging Technologies for Space (NETS) 2016, Huntsville, AL, February 22-25, 2016.

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Passivation and Stabilization of Aluminum Nanoparticles for Energetic Materials

Matthew Flannery, Journal of Nanomaterials, vol. 2015, Received 17 June 2015; Accepted 13 October 2015

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Modeling high-temperature diffusion of gases in micro and mesoporous amorphous carbon

Raghavan Ranganathan, Srujan Rokkam, Tapan Desai, Pawel Keblinski, Peter Cross, and Richard Burnes, The Journal of Chemical Physics 143, 084701 (2015).

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Optimized Heat Pipe Backup Cooling System Tested with a Stirling Convertor

Carl L. Schwendeman, Calin Tarau, Nicholas A. Schifer, John Polak, and William G. Anderson, 13th International Energy Conversion Engineering Conference (IECEC), Orlando, FL, CA, July 27-29, 2015.

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Status of the Low-Cost Radiator for Fission Power Thermal Control

Taylor Maxwell, Calin Tarau, William G. Anderson, Scott Garner, Matthew Wrosch, and Maxwell H. Briggs, 13th International Energy Conversion Engineering Conference (IECEC), Orlando, FL, CA, July 27-29, 2015.

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Water-Titanium Heat Pipes for Spacecraft Fission Power

Rebecca Hay and William G. Anderson, 13th International Energy Conversion Engineering Conference (IECEC), Orlando, FL, CA, July 27-29, 2015.

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Two-Phase Thermal Switch for Spacecraft Passive Thermal Management

Nathan Van Velson, Calin Tarau, and William G. Anderson, 45th International Conference on Environmental Systems (IECS), Bellevue, WA, July 12-16, 2015.

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Multiple Loop Heat Pipe Radiator for Variable Heat Rejection in Future Spacecraft

Nathan Van Velson, Calin Tarau, Mike DeChristopher, and William G. Anderson, 45th International Conference on Environmental Systems (IECS), Bellevue, WA, July 12-16, 2015.

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Hybrid Heat Pipes for Planetary Surface and High Heat Flux Applications

Mohammed T. Ababneh, Calin Tarau, and William G. Anderson, 45th International Conference on Environmental Systems (IECS), Bellevue, WA, July 12-16, 2015.

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Experimental Investigation on the Thermal and Hydraulic Performance of Alumina–Water Nanofluids in Single-Phase Liquid-Cooled Cold Plates

Ehsan Yakhshi-Tafti, Sanjida Tamanna and Howard Pearlman, Journal of Heat Transfer, Vol. 137, July 1, 2015

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A “Swiss-Roll” Fuel Reformer: Experiments and Modeling

Chien-Hua Chen, Bradley Richard, Ying Zheng, Howard Pearlman, Shrey Trivedi, Srusti Koli, Andrew Lawson, and Paul Ronney, “A “Swiss-Roll” Fuel Reformer: Experiments and Modeling,” 9th U. S. National Combustion Meeting, Cincinnati, OH, May 17-20, 2015.

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Effect of Porous Coating on Condensation Heat Transfer

Ying Zheng, Chien-hua Chen, Howard Pearlman, Matt Flannery and Richard Bonner. 9th International Conference on Boiling and Condensation Heat Transfer, April 26-30, 2015, Boulder, Colorado.

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High Temperature Water-Titanium Heat Pipes for Spacecraft Fission Power

Rebecca Hay and William G. Anderson, Nuclear and Emerging Technologies for Space (NETS-2015), Albuquerque, NM, February 23-26, 2015.

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Nanoscale Coating for Microchannel Cooler Protection in High Powered Laser Diodes

Tapan Desai, Matthew Flannery, Nathan Van Velson, and Philip Griffin, “Nanoscale Coating for Microchannel Cooler Protection in High Powered Laser Diodes,” Semiconductor Thermal Measurement and Management Symposium (SEMI-THERM 2015), San Jose, CA, March 16-19, 2015.

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Fuel-Flexible Hybrid Solar Coal Gasification Reactor

M. Flannery et al., "Fuel-Flexible Hybrid Solar Coal Gasification Reactor," 2014 Pittsburgh Coal Conference, Pittsburgh, PA, October 6 - 9, 2014.

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Heat Pipe Embedded Carbon Fiber Reinforced Polymer Composite Enclosures for Avionics Thermal Management

Andrew Slippey, Michael C. Ellis, Bruce Conway, and Hyo Chang Yun. SAE 2014 Aerospace Systems and Technology Conference, Cincinnati, OH, September 23-25, 2014.

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Passive Thermal Management for Avionics in High Temperature Environments

Michael C. Ellis, William G. Anderson, and Jared R. Montgomery. SAE 2014 Aerospace Systems and Technology Conference, Cincinnati, OH, September 23-25, 2014.

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Passivation of Aluminum Nanoparticles by Plasma-Enhanced Chemical Vapor Deposition for Energetic Nanomaterials

T. Desai et al., ACS Applied Materials and Interfaces Journal, 2014, 6 (10), pp. 7942–7947, DOI: 10.1021/am5012707

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Thermal Modeling and Experimental Validation for High Thermal Conductivity Heat Pipe Thermal Ground Planes

Ababneh, Mohammed T., Shakti Chauhan, Pramod Chamarthy, and Frank M. Gerner. "Thermal Modeling and Experimental Validation for High Thermal Conductivity Heat Pipe Thermal Ground Planes." Journal of Heat Transfer 136, no. 11 (2014): 112901.

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Launch Vehicle Avionics Passive Thermal Management

W. G. Anderson et al., “Launch Vehicle Avionics Passive Thermal Management,” 44th International Conference on Environmental Systems (ICES 2014), Tucson, AZ, July 13-17, 2014.

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Low Cost Radiator for Fission Power Thermal Control

Taylor Maxwell et al, 12th International Energy Conversion Engineering Conference (IECEC), Cleveland, OH, July 28-30, 2014.

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Flow Boiling Heat Transfer Enhancement in Subcooled and Saturated Refrigerants in Minichannel Heat Sinks

E. Yakhshi-Tafti et al., ASME 2014 4th Joint US-European Fluids Engineering Division Summer Meeting and 12th International Conference on Nanochannels, Microchannels, and Minichannels, August 3-7, 2014, Chicago, IL.

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Thermal-Fluid Modeling for High Thermal Conductivity Heat Pipe Thermal Ground Planes

M. T. Ababneh et al., published in the AIAA Journal of Thermophysics and Heat Transfer, Vol. 28, No. 2, pp. 270-278, April 2014.

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Thermoelectric Performance Model Development and Validation for a Selection and Design Tool

Thomas Nunnally, Devin Pellicone, Nathan Van Velson, James Schmidt, Tapan Desai, 2014 IEEE Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems (ITherm), Orlando, FL, May 27-30, 2014.

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High Heat Flux Heat Pipes Embedded in Metal Core Printed Circuit Boards for LED Thermal Management

Dan Pounds, Richard W. Bonner III, 2014 IEEE Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems (ITherm), Orlando, FL, May 27-30, 2014

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Enhancing Thermal Performance in Embedded Computing for Ruggedized Military and Avionics Applications

Darren Campo, Jens Weyant, Bryan Muzyka, 2014 IEEE Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems (ITherm), Orlando, FL, May 27-30, 2014.

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A Corrosion and Erosion Protection Coating for Complex Microchannel Coolers used in High Power Laser Diodes

Tapan G. Desai, Matthew Flannery, Angie Fan, Jens Weyant, Henry Eppich, Keith Lang, Richard Chin, and Aland Chin, 2014 IEEE Intersociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems (ITherm), Orlando, FL, May 27-30, 2014

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The Thermal Conductivity of Clustered Nanocolloids

T. Desai et al., APL Materials, 2, 066102 (2014); doi: 10.1063/1.4880975. 21 May 2014;

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Diffuse interface modeling of void growth in irradiated materials. Mathematical, thermodynamic and atomistic perspectives

Anter El-Azab Karim Ahmed, Srujan Rokkam, Thomas Hochrainer, Published in Current Opinion in Solid State and Materials Science (COSSMS), Vol. 18, pg. 90-98, 2014.

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Effect of Crosslink Formation on Heat Conduction in Amorphous Polymers

Gota Kikugawa, Tapan G. Desai, et al., Journal of Applied Physics 114, published online July 16, 2013

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Variable Conductance Heat Pipe Cooling of Stirling Convertor and General Purpose Heat Source

Calin Tarau, et al.,11th International Energy Conversion Engineering Conference (IECEC), San Jose, CA, July 15-17, 2013.

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High Temperature Heat Pipes for Space Fission Power

Kara L. Walker, et al.,11th International Energy Conversion Engineering Conference (IECEC), San Jose, CA, July 15-17, 2013.

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Variable Conductance Heat Pipe Radiator for Lunar Fission Power Systems

William G. Anderson, et al., 11th International Energy Conversion Engineering Conference (IECEC), San Jose, CA, July 15-17, 2013.

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Ammonia and Propylene Loop Heat Pipes with Thermal Control Valves – Thermal/Vacuum and Freeze/Thaw Testing

Kara Walker, et al., 43rd International Conference on Environmental Systems (ICES 2013), Vail, CO, July 14-18, 2013.

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Intermediate Temperature Heat Pipe Life Tests and Analyses

W. G. Anderson, et al., 43rd International Conference on Environmental Systems (ICES 2013), Vail, CO, July 14-18, 2013

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Correlation for dropwise condensation heat transfer: Water, organic fluids, and inclination

Richard W. Bonner III, International Journal of Heat and Mass Transfer, Volume 61, June 2013, Pages 245-253

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A Non-Catalytic Fuel-Flexible Reformer

Chien-Hua Chen, et al., 8th U. S. National Combustion Meeting, hosted by the University of Utah, May 19-22, 2013

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Planar vapor chamber with hybrid evaporator wicks for the thermal management of high-heat-flux and high-power optoelectronic devices

P. Dussinger et al., International Journal of Heat and Mass Transfer, Volume 60, pp. 163–169, May 2013.

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Variable Conductance Thermal Management System for Balloon Payloads

Calin Tarau and William G. Anderson, 20th AIAA Lighter-Than-Air Systems Technology Conference, Daytona Beach, FL, March, 25-28, 2013

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Preliminary First Principle Based Electro-thermal Coupled Solver for Silicon Carbide Power Devices

Angie Fan et al., 29th IEEE SEMI-THERM Symposium, San Jose, CA, March 17-21, 2013

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Variable Conductance Heat Pipe Radiator Trade Study for Lunar Fission Power Systems

William G. Anderson, Bryan J. Muzyka, and John R. Hartenstine, Nuclear and Emerging Technologies for Space (NETS-2013), Albuquerque, NM, February 25-28, 2013.

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Alkali Metal Backup Cooling for Stirling Systems – Experimental Results

Carl Schwendeman, Calin Tarau, William G. Anderson, and Peggy A. Cornell, Nuclear and Emerging Technologies for Space (NETS-2013), Albuquerque, NM, February 25-28, 2013.

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Alkali Metal Heat Pipes for Space Fission Power

Kara L. Walker, Calin Tarau, and William G. Anderson, Nuclear and Emerging Technologies for Space (NETS-2013), Albuquerque, NM, February 25-28, 2013.

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Syngas Production by Thermochemical Conversion of CO2 and H2O Using a High-Temperature Heat Pipe Based Reactor

H. Pearlman and Chien-Hua Chen, SPIE Solar Hydrogen and Nanotechnology VII, Proceedings of SPIE Vol. 8469 San Diego, CA, August 12-14, 2012.

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Diode Heat Pipes for Venus Landers

Calin Tarau et al., 9th Intersociety Energy and Conversion Engineering Conference (IECEC), San Diego, CA, July 31 - August 3, 2012.

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Long-Lived Venus Lander Thermal Management System Design

Rebecca Hay et al., 9th Intersociety Energy and Conversion Engineering Conference (IECEC), Atlanta, GA, July 30 July-August 1, 2012.

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Variable Conductance Heat Pipes for Variable Thermal Links

W. G. Anderson et al., 42nd International Conference on Environmental Systems (ICES 2012), San Diego, CA, July 15-19, 2012.

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Pressure Controlled Heat Pipe Applications

W. G. Anderson et al., 16th International Heat Pipe Conference, Lyon, France, May 20-24, 2012.

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The Effect of Device Level Modeling on System-Level Thermal Predictions

Jens Weyant, et al., ITherm, San Diego, CA, May 30, 2012,

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Integration of a Phase Change Material for Junction-Level Cooling in GaN Devices

Daniel Piedra, et al., Semitherm, San Jose, CA, March 2012

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An Innovative Passive Cooling Method for High Performance Light-emitting Diodes

Angie Fan, et al., Semitherm, San Jose, CA, March 2012

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Ultra High Temperature Isothermal Furnace Liners (IFLs) For Copper Freeze Point Cells

Peter Dussinger and John Tavener, 9th International Temperature Symposium, Anaheim, CA, March 2012

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High Heat Flux, High Power, Low Resistance, Low CTE Two-Phase Thermal Ground Planes for Direct Die Attach Applications

Peter Dussinger, et al., GOMACTech 2012, Las Vegas, Nevada, March 2012

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Passive Control of a Loop Heat Pipe with Thermal Control Valve for Lunar Lander Application

K. L. Walker et al., 42nd International Conference on Environmental Systems (ICES 2012), San Diego, CA, July 15-19, 2012.

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A Computational Model of a Phase Change Material Heat Exchanger in a Vapor Compression System with a Large Pulsed Heat Load

G. Troszak and X. Tang, Proceedings of the ASME 2012 Summer Heat Transfer Conference, Puerto Rico, July 8-12, 2012.

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2-D Simulation of Hot Electron-Phonon Interactions in a Submicron Gallium Nitride Device Using Hydrodynamic Transport Approach

Angie Fan et al., ASME 2012 Summer Heat Transfer Conference, Puerto Rico, USA , July 8-12, 2012

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Novel Junction Level Cooling in Pulsed GaN Devices

Tapan G. Desai, et al., ITherm, San Diego, CA, May 30, 2012,

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Intermediate Temperature Heat Pipe Life Tests

W. G. Anderson, et al., 16th International Heat Pipe Conference, Lyon, France, May 20-24, 2012.

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Passivation Coatings for Micro-channel Coolers

Richard W. Bonner III, Jens Weyant, Evan Fleming, Kevin Lu, Daniel Reist, APEC 2012, Orlando FL, February 1, 2012

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Pressure Controlled Heat Pipe Solar Receiver for Regolith Oxygen Production with Multiple Reactors

John Hartenstine, et al., 9th Intersociety Energy and Conversion Engineering Conference (IECEC), San Diego, CA, July 31 - August 3, 2011

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Thermal Management System for Long-Lived Venus Landers

Calin Tarau, et al., 9th Intersociety Energy and Conversion Engineering Conference (IECEC), San Diego, CA, July 31 - August 3, 2011

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Pressure Controlled Heat Pipes

William Anderson, et al., 41st International Conference on Environmental Systems, Portland, OR, July 17-21, 2011

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Variable Conductance Heat Pipe for a Lunar Variable Thermal Link

Chris Peters, et al., 41st International Conference on Environmental Systems, Portland, OR, July 17-21, 2011

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Two-Phase Heat Sinks with Microporous Coating

T. Semenic and S. M. You, 9th International Conference on Nanochannels, Microchannels, and Minichannels, Edmonton, CA, June 19-22, 2011

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Die Level Thermal Storage for Improved Cooling of Pulsed Devices

Richard Bonner III, et al., Semitherm, San Jose, CA., March 2011

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A 2-D Numerical Study of Microscale Phase Change Material Thermal Storage for GaN Transistor Thermal Management

Xudong Tang, et al., Semitherm, San Jose, CA, March 2011

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Dynamic Response of Phenolic Resin and Its Carbon-nanotube Composites to Shock Wave Loading

Arman, et. al., Journal of Applied Physics, 109, 013503 (2011)

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Loop Heat Pipe with Thermal Control Valve for Variable Thermal Conductance Link of Lunar Landers and Rovers

Loop Heat Pipe with Thermal Control Valve for Variable Thermal Conductance Link of Lunar Landers and Rovers, J. R. Hartenstine et al., 49th AIAA Aerospace Sciences Meeting, Orlando, FL, January 4-7, 2011.

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Electronics Cooling Using High Temperature Loop Heat Pipes with Multiple Condensers

William G. Anderson, et al., SAE Power Systems Conference, Ft. Worth, TX, November 2010

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Development of Heat Pipe Loop Technology for Military Vehicle Electronics Cooling

Xudong Tang et al., NDIA Ground Vehicle Systems Engineering and Technology Symposium, Dearborn, Michigan, August 2010

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Dropwise Condensation Life Testing of Self Assembled Monolayers

Richard Bonner III, IHTC14, Washington, DC, August 2010

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Heat and Mass Transfer in a Permeable Fabric system Under Hot Air Jet Impingement,

Sangsoo Lee et. al., International Heat Transfer Conference (IHTC14), Washington, DC, August, 2010

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Variable Thermal Conductance Link for Lunar Landers and Rovers

William G Anderson et. al., IECEC, Nashville, Tennessee, July, 2010

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Sodium Variable Conductance Heat Pipe for Radioisotope Stirling Systems – Design and Experimental Results

Calin Tarau and William G Anderson, IECEC, Nashville, Tennessee, July, 2010

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Sodium Variable Conductance Heat Pipe with Carbon-Carbon Radiator for Radioisotope Stirling Systems

Calin Tarau and William G. Anderson, 15th International Heat Pipe Conference, Clemson, SC, April 2010

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Low-Temperature, Dual Pressure Controlled Heat Pipes for Oxygen Production from Lunar Regolith

Kara Walker et al., 15th International Heat Pipe Conference, Clemson, South Carolina, April, 2010

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Intermediate Temperature Fluids for Heat Pipes and Loop Heat Pipes

William G. Anderson, John R. Hartenstine, David B. Sarraf, and Calin Tarau, Advanced Cooling Technologies, Inc., Pennsylvania, 15th International Heat Pipe Conference (15th IHPC) Clemson, USA, April 25-30, 2010.

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Dropwise Condensation in Vapor Chambers

Richard Bonner, 26th IEEE Semi-Therm Symposium, Santa Clara, California, February 2010

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Sodium VCHP with Carbon-Carbon Radiator for Radioisotope Stirling Systems,

Calin Tarau, et al., Space, Propulsion and Energy Sciences International Forum (SPESIF), Laurel, Maryland, February 2010

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Advanced VCS Evaporators for Lunar Lander and Lunar Habitat Thermal Control Applications

Tadej Semenic, Space, Propulsion and Energy Sciences International Forum (SPESIF), Laurel, Maryland, February 2010

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Modeling Initial Stage of Phenolic Pyrolysis: Graphitic Precursor Formation and Interfacial Effects

Tapan Desai, et al., Polymer, 52, 2010

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Slip Behavior at Ionic Solid-fluid Interfaces

Tapan Desai, NDIA Chemical Physics Letters, 501, 2010, 93-97

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Roles of Atomic Restructuring in Interfacial Phonon Transport

Seungha Shin et. al., Physical Review B, 82, 081302 (2010)

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Anisotropic Shock Response of Columnar Nanocrystalline Cu

Sheng-Nian Luo et. al., Journal of Applied Physics , 107, 123507 (2010)

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Heat Pipe Embedded Alsic Plates for High Conductivity-Low CTE Heat Spreaders

J. Weyant, ITHERM 2010, Las Vegas NV,

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Pressure Controlled Heat Pipe Solar Receiver for Oxygen Production from Lunar Regolith

John R. Hartenstine, et al., AIAA Aerospace Sciences Meeting, Orlando, Florida, January 2010

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Sodium Variable Conductance Heat Pipe for Radioisotope Stirling Systems

Calin Tarau, et al., 7th International Energy Conversion Engineering Conference, Denver Colorado, August 2009

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Loop Heat Pipe Design, Manufacturing and Testing – an Industrial Perspective

William Anderson, et al., ASME 2009 Heat Transfer Summer Conference, San Francisco, California, July 2009

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Dropwise Condensation on Surfaces with Graded Hydrophobicity

Richard Bonner, ASME 2009 Heat Transfer Summer Conference, San Francisco, California, July 2009

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Evaporators for High Temperature Lift Vapor Compression Loop for Space Applications

Tadej Semenic and Xudong Tang, ASME 2009 Heat Transfer Summer Conference, San Francisco, California, July 2009

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Variable Conductance Heat Pipe Radiators for Lunar and Martian Environments

William Anderson, et al., Space, Propulsion and Energy Sciences International Forum (SPESIF), Huntsville, Alabama, February 2009

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High Temperature Variable Conductance Heat Pipes for Radioisotope Stirling Systems

Calin Tarau, et al., Space, Propulsion and Energy Sciences International Forum (SPESIF), Huntsville, Alabama, February 2009

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Heat Pipe Solar Receiver for Oxygen Production of Lunar Regolith

John Hartenstine, et al., Space, Propulsion and Energy Sciences International Forum (SPESIF), Huntsville, Alabama, February 2009

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Variable Conductance Heat Pipe Performance after Extended Periods of Freezing

Michael Ellis and William Anderson, Space, Propulsion and Energy Sciences International Forum (SPESIF), Huntsville, Alabama, February 2009

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Loop Heat Pipe for TacSat-4

Peter Dussinger, et al., Space, Propulsion and Energy Sciences International Forum (SPESIF), Huntsville, Alabama, February 2009

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Advanced Thermal Management Technologies for High Power Automotive Equipment

Jon Zuo, et al., National Defense Industrial Association Ground Vehicle Power and Energy Workshop, Troy, Michigan, November 2008

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Vibration and Shock Tolerant Capillary Two-Phase Loop Technology for Vehicle Thermal Control

Xudong Tang and Chanwoo Park, 2008 ASME Summer Heat Transfer Conference, Jacksonville, Florida, August 2008

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NaK Variable Conductance Heat Pipe for Radioisotope Stirling Systems

Calin Tarau, et al., 6th International Energy Conversion Engineering Conference (IECEC), Cleveland, Ohio, July 2008

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Heat Pipe Cooling of Concentrating Photovoltaic (CPV) Systems

William Anderson, et al., 6th International Energy Conversion Engineering Conference (IECEC), Cleveland, Ohio, July 2008

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Startup Characteristics and Gravity Effects on a Medium/High-Lift Heat Pump Using Advanced Hybrid Loop Technology

Eric Sunada, et al., 38th SAE International Conference on Environmental Systems, San Francisco, California, June 2008

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High Temperature and High Heat Flux Thermal Management for Electronics

David Sarraf and William Anderson, IMAPS International Conference on High Temperature Electronics Conference (HiTEC 2008), Albuquerque, New Mexico, May 2008

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Heat Pipe Cooling of Concentrating Photovoltaic Cells

William Anderson, et al., 33rd IEEE Photovoltaic Specialists Conference, San Diego, California, May 2008

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Local Heat Transfer Coefficient Measurements of Flat Angled Sprays Using Thermal Test Vehicle

Richard Bonner, et al., 24th IEEE Semi-Therm Symposium, San Jose, California, March 2008

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Pressure Controlled Heat Pipe for Precise Temperature Control

David Sarraf, et al., Space Technology and Applications International Forum (STAIF), Albuquerque, New Mexico, February 2008

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Titanium Loop Heat Pipes for Space Nuclear Power Systems

John Hartenstine, et al., Space Technology and Applications International Forum (STAIF), Albuquerque, New Mexico, February 2008

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Variable Conductance Heat Pipes for Radioisotope Stirling Systems

William Anderson and Calin Tarau, Space Technology and Applications International Forum (STAIF), Albuquerque, New Mexico, February 2008

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Vapor Compression Hybrid Two-Phase Loop Technology for Lunar Surface Applications

Chanwoo Park and Eric Sunada, Space Technology and Applications International Forum (STAIF), Albuquerque, New Mexico, February 2008

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Experimental Study of Oscillating Flow Heat Transfer

Angie Fan, et al., Micro/Nanoscale Heat Transfer International Conference, Tainan, Taiwan, January 2008

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Metal Hydride Heat Storage Technology for Directed Energy Weapon Systems

Chanwoo Park, et al., 2007 ASME International Mechanical Engineering Congress & Exhibition, Seattle, Washington, November 2007

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Electronics Thermal Management Using Advanced Hybrid Two-Phase Loop Technology

Chanwoo Park, et al., 2007 ASME-JSME Thermal Engineering Summer Heat Transfer Conference, Vancouver, Canada, July 2007.

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Loop Thermosyphon Design for Cooling of Large Area, High Heat Flux Sources

John Hartenstine, et al., InterPACK 2007, Vancouver, Canada, July 2007.

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Heat Pipes for High Temperature Thermal Management

David Sarraf and William Anderson, InterPACK 2007, Vancouver, Canada, July 2007.

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Intermediate Temperature Fluids for Heat Pipes and Loop Heat Pipes

William Anderson, 2007 International Energy Conversion Engineering Conference, St. Louis, MO, June 2007.

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Intermediate Temperature Fluids Life Tests – Experiments

William Anderson, et al., 2007 International Energy Conversion Engineering Conference, St. Louis, MO, June 2007.

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Intermediate Temperature Fluids Life Tests – Theory

Calin Tarau, et al., Space Technology and Applications International Forum (STAIF), Albuquerque, NM, February 11 - 15, 2007.

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Spacecraft Thermal Management Using Advanced Hybrid Two-Phase Loop Technology

Chanwoo Park, et al., Space Technology and Applications International Forum (STAIF), Albuquerque, NM, February 11 - 15, 2007.

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Advanced Hybrid Cooling Loop Technology for High Performance Thermal Management

Chanwoo Park, et al., 2006 International Energy Conversion Engineering Conference, San Diego, CA, June 2006.

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Heat Pipe Heat Exchanger with Two Levels of Isolation for Environmental Control of Manned Spacecraft Crew Compartment

David Sarraf, 37th International Conference on Environmental Systems, Norfolk, VA, July 17-20, 2006.

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Passive Thermal Management for a Fuel Cell Reforming Process

David Sarraf, et al., 2006 International Energy Conversion Engineering Conference, San Diego, CA, June 2006.

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High Temperature Water-Titanium Heat Pipe Radiator

William Anderson, et al., 2006 International Energy Conversion Engineering Conference, San Diego, CA, June 2006.

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High Temperature Titanium-Water and Monel-Water Heat Pipes

William Anderson, et al., 2006 International Energy Conversion Engineering Conference, San Diego, CA, June 2006.

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High-Temperature Water Heat Pipes

David Sarraf and William Anderson, IMAPS International Conference on High Temperature Electronics, Santa Fe, NM, May 15 - 18, 2006

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High Performance Heat Storage and Dissipation Technology

Chanwoo Park, et al., 2005 ASME International Mechanical Engineering Congress & Exposition (IMECE), Orlando, FL, November 5 - 11, 2005.

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Design and Testing of Titanium/Cesium and Titanium/Potassium Heat Pipes

Peter Dussinger, et al., 2005 International Energy Conversion Engineering Conference (IECEC), San Francisco, CA, August 2005.

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High Temperature Lightweight Heat Pipe Panel Technology Development

Ted Stern and William Anderson, Space Nuclear Conference 2005, San Diego, CA, June 2005.

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Loop Heat Pipe Radiator Trade Study for the 300-550K Temperature Range

William Anderson and Walter Bienert, Space Technology and Applications International Forum (STAIF), Albuquerque, New Mexico, February 2005

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Hybrid Loop Thermal Bus Technology for Vehicle Thermal Management

Chanwoo Park, et al., 24th Army Science Conference, Orlando, FL, November 29 - December 2, 2004

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