List of people whom supported TFAWS 2022!
Link to YouTube playlist containing TFAWS 2022 recordings
The TFAWS 2022 Proceedings are included below. The proceedings can be navigated by using the shortcuts below, or by using the “Ctrl+F” search feature to search by title, paper identifier, or author.
Active Thermal Papers and Presentations
Aerothermal Papers and Presentations
Cryogenics Papers and Presentations
Interdisciplinary Papers and Presentations
Passive Thermal Papers and Presentations
Short Courses (only publicly available courses are listed)
Active Thermal Paper Sessions
Session Chairs:
Michael Elmore, NASA Kennedy Space Center
Tom Leimkuehler, NASA Johnson Space Center
Active Thermal Paper Session, Tuesday, 9:00-12:00
| TFAWS22-AT-01 | Simulation of Heat Transfer of Al2O3/Water Nanofluid- Effect Volume Fraction AmirReza-Radmanesh and Nihad Dukhan |
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| TFAWS22-AT-02 | Transformative Particle Enhanced Active Cooling Control System Without Pumping Penalty Jose Lage, and Amir Kiaee |
| TFAWS22-AT-03 | Development of Thermal Corer for Ice-Extraction for ISRU Applications Sai Kiran Hota, Kuan-Lin Lee, Quang Truong, and Kris Zacny |
| TFAWS22-AT-05 | Design of the thermal control system for the ULTRASAT camera Juan Maria Haces Crespo, and Merlin Barschke |
Aerothermal Paper Session
Session Chairs:
William Dziedzic, NASA Kennedy Space Center
Jonathan Pitt, NASA Kennedy Space Center
JB (James) Scoggins, NASA Langley Research Center
Adam Wise, NASA Langley Research Center
Aerothermal Paper Session 1: Applications, Tuesday, 13:00-16:00
| TFAWS22-AE-01 | Overview of Recent (2019-2022) Langley Aerothermodynamic Laboratory Tests at NASA Langley Research Center Michelle Mason Presentation not publicly available. NASA Technical Reports Server (NTRS) link only. |
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| TFAWS22-AE-02 | Characterizing Char Rate and Extent in Fiber-Reinforced Plastics Using X-ray Computed Tomography Benton Greene, and Chris Ostrom |
| TFAWS22-AE-03 | Arc Jet Assessment of MEDLI2 Radiometer Window Blockage Due to TPS Ablation Product Deposits Ruth Miller, Brett Cruden, Jose Santos, and Todd White |
| TFAWS22-AE-04 | High-fidelity modeling and validation of a re-entry capsule in earth atmosphere including wall catalysis Erick Martinez, Valerio Viti, Song Gao, and Henry Vu |
| TFAWS22-AE-05* | Overview of Mars Sample Return Earth Entry System Aerothermodynamics Christopher Johnston |
| TFAWS22-AE-06 | Towards the Prediction of Entry Capsule Dynamic Stability Characteristics with Reduced Free Flight Motion in FUN3D Eli Shellabarger |
Aerothermal Paper Session 2: Computational Development, Wednesday, 13:00-16:00
| TFAWS22-AE-07 | Computation of Effective Mechanical Properties and Mechanical Erosion Modeling of TPS Materials Sergio Fraile Izquierdo, Jeremie B.E. Meurisse, Federico Semeraro, Georgios Bellas Chatzigeorgis, Marcos Acin, and Nagi N. Mansour |
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| TFAWS22-AE-09* | An overview of recent developments and applications of the Icarus material response code Joseph Schulz |
| TFAWS22-AE-10 | Derivation and development of a unified flow-material solver Bruno Dias, Aleksander Zibitsker, Jeremie Meurisse, and Nagi Mansour |
| TFAWS22-AE-11 | Mean Flow Effects on Hypersonic Boundary-Layer Stability Analysis using LASTRAC Xiaowen Wang, Chau-lyan Chang, and Fei Li |
| TFAWS22-AE-12 | Accelerating Steady-State Convergence of Compressible Flow Simulations via Nonlinear Elimination Kyle Thompson, Matthew O’Connell, and Cameron Druyor |
Cryogenics Paper Session
Session Chairs:
Monica Guzik, NASA Glenn Research Center
Brett Warner, NASA Goddard Space Flight Center
Chris Evans, NASA Goddard Space Flight Center
Cryogenics Paper Session, Thursday, 14:00-16:00
| TFAWS22-CT-01 | An Equation-free Based Coupling Approach for Long-term Cryogenic Tank Behavior Predictions Qiyun Cheng, Shanbin Shi, Michael Harris, Mamoru Ishii, and Wei Ji |
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| TFAWS22-CT-02 | Analytical Study of a Cryogenic Thermal Control Coating Jarred Wilhite, and Justin Elchert |
| TFAWS22-CT-03 | A dynamic adaptive mesh refinement and space-time spectral element method for improved capturing of vortical structures in a realistic Cryogenic Fuel tank Mark Sussman, Yang Liu, Cody Estebe, Mehdi Vahab, Alireza Moradikazerouni, Kourosh Shoele, and Wei Guo |
| TFAWS22-CT-04 | Liquid Nitrogen Testing of an Integrated Reaction Control System Anson Koch, and Hannah Cherry |
| TFAWS22-CT-05 | Measurements and Correlations for Critical Heat Flux in Cryogenic Boiling Mike Izenson, Lucas O’Neill, Chirag Kharangate, and Jiayuan Li |
| TFAWS22-CT-06 | Cryogenic Fluid Management (CryoFM) Tool for Systems Analysis and Design Matthew Moran |
ITAR Paper Sessions
ITAR Paper Sessions are restricted to US Citizens and US Lawful Permanent Residents only, and are not publicly available for posting. If you are a US Citizen or Lawful Permanent Resident and wish to view the session content, please request it through the authors’ institutions/agencies directly. Note: There were no ITAR Paper sessions for TFAWS 2022.
Interdisciplinary Paper Sessions
Session Chairs:
Michael Elmore, NASA Kennedy Space Center
Tom Leimkuehler, NASA Johnson Space Center
Interdisciplinary Paper Session 1: Computational, Wednesday, 10:00-12:00
| TFAWS22-ID-01 | Additively Manufactured Heat Pipes Payton Batliner, and Alex Pagano |
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| TFAWS22-ID-02 | Benchmarking Performance of Machine Learning Algorithms for Fluid Flow Simulation by Leveraging Cluster Computing: A Case Study for High Performance Computing Devkumar Banerjee, and Debjyoti Banerjee |
| TFAWS22-ID-03 | Leveraging Machine Learning (ML) and Advanced Manufacturing (AM) for Enhancing Thermal Energy Storage (TES) using Molten Salt Nanofluids and Phase Change Materials (PCM) Debjyoti Banerjee |
Session Chairs:
Monica Guzik, NASA Glenn Research Center
Brett Warner, NASA Goddard Space Flight Center
Chris Evans, NASA Goddard Space Flight Center
Interdisciplinary Paper Session 2, Friday, 13:00-16:00
| TFAWS22-CT-09 | Smart Propellant Tanks, gauging and slosh force measurement using Electrical Capacitance Tomography Andrew Hunt, and Richard Foster-Turner |
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| TFAWS22-CT-10 | Preliminary Results from Propellant Mass Gauging in Microgravity with Electrical Capacitance Tomography Jed Storey, Brandon Marsell, Mike Elmore, and Scott Clark |
| TFAWS22-ID-05 | Thermal Sizing of a Lunar Rover using SimCenter 3D Jean-Francois Labrecque |
| TFAWS22-ID-06 | Excel Based Tool For Spacecraft Thermal Design Kevin Anderson, and Ariel Gatti |
| TFAWS22-ID-07 | Enhanced thermal-structural analysis using reduced-order modeling Derek Hengeveld |
Passive Thermal Paper Sessions
Session Chairs:
Melissa Young, NASA Kennedy Space Center
Jared Congiardo, NASA Kennedy Space Center
Evan Racine, NASA Glenn Research Center
Passive Thermal Paper Session 1, Thursday, 9:00-12:00
| TFAWS22-PT-02 | Lightweight Liquid Metal Elastomer Composites for Passive Thermal Management Eric Markvicka |
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| TFAWS22-PT-03 | Measuring the Performance of Thermal Interface Materials in an In-situ Test Environment Andras Vass-Varnai, and Weikun-Jimmy HE |
| TFAWS22-PT-04 | Passively Deployed, Unfolding Radiator Panels for Small Satellite Thermal Management Josh Cannon, Rydge Mulford, and Brian Iverson |
| TFAWS22-PT-06 | Manual and Automated Thermal Model Correlation Methods for JPL SWOT Mission Lina Maricic |
| TFAWS22-PT-07 | Advanced Thermal Radiator for Global Lunar Heat Rejection Jodi Turk |
| TFAWS22-PT-08 | Thermal Management for Lunar Landers and Rovers William Anderson, Richard Bonner, Jeffrey Diebold, Michael Ellis, Ion Nicolaescu, Nathan Van Velson, Calin Tarau, Jianjian Wang, Troy Arbuckle, and Robert Rolley |
Passive Thermal Paper Session 2: Heat Pipes and Cold Plates, Friday, 9:00-12:00
| TFAWS22-PT-17 | Practical Alternative for Diffusing Constructal Network Enhanced Coldplates Jose Lage |
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| TFAWS22-PT-10 | High Temperature Oscillating Heat Pipe Radiators for Management of Fission Power Generation Alex Miller, and Shane Hilsenbeck |
| TFAWS22-PT-11 | Additive Oscillating Heat Pipe Development for Electric Aircraft Thermal Management System and Waste Heat Recovery Patrick Margavio, and Scott Hayden |
| TFAWS22-PT-12 | Optimal design solutions of innovative Aero-Thermo-Structural Design with advances OHP/PHP for next generation spacecraft development technology into NASA Missions Shamsuddin Khaled |
| TFAWS22-PT-13 | High Temperature Oscillating Heat Pipe for Leading Edge Applications Alex Miller, and Dan Pounds |
| TFAWS22-PT-14 | Non-Integrated Hot Reservoir Variable Conductance Heat Pipes for Lunar Surface Applications Jeff Diebold, Calin Tarau, Joshua Smay, Timothy Hahn, and Ryan Spangler |
| TFAWS22-PT-15 | Advanced Hot Reservoir Variable Conductance Heat Pipe with Enhance Reliability Kuan-Lin Lee |
| TFAWS22-PT-16 | Advanced Two-Phase Cooling System for Modular Power Electronics Sai Kiran Hota, and Kuan-Lin Lee |
| TFAWS22-PT-18 | Development of a Large, Variable Conductance Cold Plate for Spatial and Temporal Isothermality Jana Catuche, Elizabeth Seber, Michael Ellis, and Haley Myer |
Short Courses
| Form Factors, Grey Bodies, and Radiation Conductances, Tuesday, 10:00-12:00 and 13:00-15:00, Video Steve Rickman, NASA NESC Thermal radiation is often the predominant heat transfer mode in space-related thermal analysis. A variety of techniques are employed in commonly available analysis tools. This short course focuses on the role of form factors, grey body factors, and radiation conductances in thermal radiation analysis and is designed to provide students insight into how these important quantities are calculated. Students are introduced methods for form factor calculation including double area summation, Nusselt sphere, and monte carlo techniques. Grey body factors are introduced and calculated using radiosity and monte carlo techniques. Statistical error for, both, monte carlo form factor and interchange factor calculations is discussed. Transformation of the grey body factors into radiation conductances is demonstrate. |
| An Overview of Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology, Tuesday, 12:00-13:00, Video Neil Cheatwood Entry mass at Mars, and other destinations with atmospheres, is limited by the aeroshell size that can fit in the launch vehicle fairing. A Hypersonic Inflatable Aerodynamic Decelerator (HIAD) is a deployable aeroshell consisting of an inflatable structure that maintains shape during atmospheric flight, and a flexible thermal protection system which protects the entry vehicle through hypersonic entry. HIAD is stowed for launch and then inflated prior to atmospheric interface. |
| Lunar Thermal Analysis Guidebook (L-TAG), Wednesday, 10:00-12:00 and 13:00-15:00, Video Greg Schunk, Carlos Gomez, Brian Hamill, and Lisa Erickson The purpose of the Human Landing System (HLS) Lunar Thermal Analysis Guidebook (L-TAG) is to provide guidance to experienced thermal engineering personnel on how to conduct worst-case hot and cold lunar thermal analyses for the design of HLS hardware in both lunar orbit and lunar surface environments. The HLS L-TAG will include pointers to the Cross-Program Design Specification for Natural Environments (DSNE), SLS-SPEC-159, and best practices/approaches for interpreting and complying with the DSNE lunar thermal environments in the analysis of HLS spacecraft, vehicles and systems. The HLS L-TAG is a reference document that is available to all HLS thermal analysts. In the event of a conflict with the descriptions provided herein, the DSNE takes precedence. This document represents the best available information at the time of publication and will undergo updates as the HLS program evolves. Feedback from the user community is encouraged to support further refinement of the Guidebook. |
| Passive Cryogenic Fluid Management, Thursday, 9:00-12:00, Video Matt Moran The objective of this short course is to provide insights, methods, equations, and algorithms for passive cryogenic fluid management (CFM) techniques and operations suitable for performing initial system designs and trades. The calculations presented yield order of magnitude (zeroth-order) or first-order approximations for quick assessments and to complement higher fidelity models that require more time and resources to generate results. |
| CFD for Capsule Design, Thursday, 13:00-16:00, Video Dinesh Prabhu The role of CFD in the aerothermal design of capsules for entry into the atmospheres of Ice Giant planets – Uranus and Neptune – is explored. Starting with the atmospheric model/structure, models are developed for numerical integration of the governing equations. Wall boundary conditions with variations are discussed. An example for Uranus entry is provided as a basis for discussion. Finally, the use of CFD to develop scaling laws to incorporate into trajectory codes for rapid trades in initial concept design is discussed. |
| Rapid Thermal Design, Modeling, and Analysis of Spaceflight Instruments, Friday, 9:00-11:00, Video Kan Yang This course is intended to provide a general overview of how to conduct rapid thermal design, modeling, and analysis of spaceflight instruments for early concept studies and proposal development. The course will cover the rapid thermal design process, including obtaining thermal requirements, building a preliminary model, and iterating technical design with other engineering disciplines. It will also provide specific design guidelines for categories of instruments at different ranges on the electromagnetic spectrum. Tall poles or lessons learned will be addressed for each instrument design example. |
Cryogenics Panel Discussion, Thursday, 13:00-14:00, Video
| Olga Kartuzova, NASA Glenn Research Center / Case Western Reserve University Daniel Hauser, NASA Glenn Research Center Alok Majumdar, NASA Marshall Space Flight Center Matthew Moran, NASA Glenn Research Center Cindy Fortenberry, NASA Kennedy Space Center Jacob Roth, NASA Kennedy Space Center |