Paper #	Session	Session Chair	Title	Authors	Affiliation	View Presentation	View Paper
TFAWS-04-1001	Thermal Software	Ruth Amundsen (NASA/LaRC)	Use of the Interface-Backload method for Solving LISA and other Large, Divided Thermal Problems	Hume Peabody	Swales Aerospace		X
TFAWS-04-1003	Thermal Software		Using UGS I-deas TMG? to Support Legacy SINDA/TRASYS models	R. Scott Miskovish	ATA Engineering, Inc		X
TFAWS-04-1004	Thermal Software		Some Impacts of Mesh Density on the Accuracy of Finite Difference Thermal Model Results	Perry Ramsey	ITT Industries	X
TFAWS-04-1005	Thermal Software		Online parameter estimation applied to mixed conduction/radiation heat transfer.	Tejas Shah	Spacecraft Technology Center-Texas A&M University		X
TFAWS-04-1006	Thermal Software		Numerical Modeling of Conjugate Heat Transfer in Fluid Network	Alok Majumdar	NASA/Marshall Space Flight Center		X
TFAWS-04-1007	Thermal Software		Numerical Modeling of Nucleation Boiling in Thin Film of Liquid and Effect of Droplet Impact	R. Panneer Selvam	University of Arkansas		X
TFAWS-04-1008	Thermal Hardware	Glenn Tsuyuki (NASA/JPL)	A Methodology for Measuring Thermal Properties of Spacecraft Bearings in Motion	Y. R. Takeuchi	The Aerospace Corporation		X
TFAWS-04-1009	Thermal Hardware		Design and Analysis of the Thermal Control System for the Space Technology 5 Microsatellite	David Neuberger	Swales Aerospace	X	X
TFAWS-04-1010	Thermal Hardware		A Simple Representation of the Impact of a Loop Heat Pipe on a Space System	Perry Ramsey	ITT Industries	X
TFAWS-04-1011	Thermal Hardware		Pressure Drop and Temperature Drop Analysis of the Optimal Top Cap Design of Evaporator of the Micro Loop Heat Pipe	PraveenKumar Arragattu	University of Cincinnati		X
TFAWS-04-1012	Thermal Hardware		Nucleate Boiling Study Inside the Evaporator of Planar Loop Heat Pipe	Junwoo Suh	University of Cincinnati		X
TFAWS-04-1013	Thermal Hardware		Long Term Characterisation of the Ulysses Reaction Control System	Colin Goulding	NASA JPL		X
TFAWS-04-1014	Thermal Hardware		Thermal Analysis Of A Mems Based Broadband Light Source: Test Data And Model	Eric Golliher	NASA GRC		X
TFAWS-04-1015	Aerothermal/CFD	Gerald Russell (US Army)	Hyper-X Hot Structures Correlation of Thermal Analysis and Flight Data	Walt Bruce	NASA Langley Research Center		X
TFAWS-04-1016	Aerothermal/CFD		CFD Analysis of Inlet and Outlet Regions of Coolant Channels in an Advanced Hydrocarbon Engine Nozzle	Kevin Anderson	Cal Poly Pomona	X	X
TFAWS-04-1017	Aerothermal/CFD		A Model for Melting Ablation in Hypersonic Heating	Tse-Fou Zien	Naval Surface Warfare Center		X
TFAWS-04-1018	Aerothermal/CFD		Aeroheating Analysis for Planetary Re-entry Vehicles	Alvin Murray	ITT Aerotherm		X
TFAWS-04-1019	Aerothermal/CFD		NASA Reentry Material Technology Test and Evaluation	Gerald Russell	US Army	X
TFAWS-04-1020	Aerothermal/CFD		Comparison Of Engineering Level and Full Navier Stokes Predictions With Test Data At The Navy?s Hot Gas Blowdown Facility T-Range	Ron Schultz	Naval Air Warfare Center	X
TFAWS-04-1021	Aerothermal/CFD		Progress in Fielding a Zero-Focus Shadowgraph System for Ablation Measurement during Arc Jet Testing	Peter Sherrouse	Aerospace Testing Alliance, AEDC	X
TFAWS-04-1023	Aerothermal/CFD		Commerical Upgraded Military Heritage Re-entry Vehicle Thermal Sensors for Current Generation TPS Ground & Flight Evaluation	John M. Cassanto	Astrometrics Inc.	X
TFAWS-04-1024	Aerothermal/CFD		Status of Advanced Two Phase Flow Model Development for SRM Chamber Flow Field and Combustion Modeling	Gary Luke	Aerojet	X
TFAWS-04-1025	Aerothermal/CFD		Status of Advanced Boundary Layer Code Development for SRM Nozzle Ablation Including Two Phase Flow Effects	Brian Mclaughlin	Aerojet	X