NASA/CP—2002–210784

Thermal and Fluids Analysis Workshop 2002

Lyndon B. Johnson Space Center
Houston, Texas

 

 

Proceedings of a workshop
hosted by the Lyndon B. Johnson Space Center
at the University of Houston Clear Lake
Houston, Texas
August 12-16, 2002

 

 

 

National Aeronautics and
Space Administration

Lyndon B. Johnson Space Center
Houston, Texas 77058

 

 

FOREWORD

The 2002 Thermal and Fluids Analysis Workshop (TFAWS) was sponsored by the NASA/Johnson Space Center and held at the University of Houston–Clear Lake campus. This was the second time that JSC has had the honor of hosting the conference; the last time was in 1997.

The workshop brought together engineers from around the world who work in industry, academia, and government. The theme for TFAWS 2002 was "Concurrent Engineering: Pushing the Limits." Four paper sessions showcased papers from a variety of disciplines: Thermal Analysis, Fluid Analysis, Propulsion Systems, and Interdisciplinary Analysis.

The organizers of this year’s workshop want to thank all of the participants, paper authors, and vendor representatives. The opportunity to coordinate the conference has been a great experience.

 


TABLE OF CONTENTS

THERMAL PAPER SESSION
Chairs: J. Saiz, NASA/Johnson Space Center
Dr. E. Ungar, NASA/Johnson Space Center

A Simplified, Closed-Form Method for Screening Spacecraft Orbital Heating Variations
S. L. Rickman, NASA/ Johnson Space Center

Use of TSS as a Neutral Format For Geometry Model Conversions: an Alternative to STEP-TAS
H. Peabody, Swales Aerospace

Thermal Orbital Environmental Parameter Study on the Propulsive Small Expendable Deployer System (ProSEDS) Using Earth Radiation Budget Experiment (ERBE) Data
John R. Sharp, NASA/Marshall Space Flight Center

Evolving the Fluids Integrated Rack (FIR) Thermal Control System Model from an Analysis Tool to a Design and Decision Tool
Paul Gebby, Northrop Grumman

Modeling of Multi-Layer Insulation Layups with Transmissive Outer Layers
Eugene K. Ungar, NASA/Johnson Space Center

Wireless Temperature Sensors for Health Monitoring of Aerospace Thermal Protection Systems
F. Milos, NASA/Ames Research Center
J. Pallix, NASA/Ames Research Center

Fundamental Study of Heat Pipe Design for High Heat Flux Source
Ryoji Oinuma, Texas A&M University
Frederick R. Best, Texas A&M University

Near-Real Time Thermal Model Matching on the Shuttle
Hensley, I. Carron, C. Akram, U. Abbas, S. Shashikant
C
ommercial Space Center for Engineering/Texas A&M University

 

 

FLUIDS PAPER SESSION
Chair: Barbara Sakowski, NASA/Glenn Research Center

The Fractional Step Method Applied to Simulations of Natural Convective Flows
Douglas G. Westra, NASA/Marshall Space Flight Center
Dr. Juan C. Heinrich, Professor of Aerospace and Mechanical Engineering Department
University of Arizona

Vortex Phase Separation in Microgravity
David Bean, Cable Kurwitz
Dr. Fredrick Best, Purvi Waghela
Department of Nuclear Engineering, Texas A&M University

Interfacing Sinda/Fluint with Rocets
Barbara Sakowski
NASA/Glenn Research Center

ORSAT Parametric Study
Christopher B. Madden
NASA/Johnson Space Center

 



PROPULSION PAPER SESSION
Chair: Eric Hurlbert, NASA/Johnson Space Center


Numerical Modeling of Cavitating Venturi – A Flow Control Element of Propulsion System
Alok Majumdar, NASA/Marshall Space Flight Center (Thermodynamics & Heat Transfer Group)

Auxiliary Propulsion System Analysis Tool (APSAT) for Sizing Vehicles
Kris Romig, NASA/Johnson Space Center (Propulsion and Fluid Systems Branch)

Non-Toxic Auxiliary Propulsion System Modeling of Liquid Oxygen Tank and Accumulator for Ground Tests
Kevin J. Miller
Eric Hurlbert
NASA/Johnson Space Center (Propulsion and Fluid Systems Branch)

Cryogenic RCS Feedsystem Test and Analysis
Kris Romig
Kevin J. Miller
Eric Hurlbert
NASA/Johnson Space Center (Propulsion and Fluid Systems Branch)

In-Situ Resource Utilization Thermal, Fluids, and Process Modeling
Tom Simon, NASA/Johnson Space Center (Propulsion and Fluid Systems Branch)

 

 

INTERDISCIPLINARY PAPER SESSION
Chair: Georg Siebes, Jet Propulsion Laboratory

Integration of Thermal Analysis in the ESA Concurrent Design Facility
Hans Peter de Koning, ESA/ESTEC
Andrea Santovincenzo, ESA/ESTEC

SMVT CDC Thermal Module: A Paradigm Shift
Saul Miller, The Aerospace Corporation

Advanced Spacecraft Conceptual Design Process at JPL
Robert Miyake, Jet Propulsion Laboratory

Utilization of Integrated High-End Analysis and Design Tools Real-Time Concurrent Design Environments
Knut Oxnevad, Jet Propulsion Laboratory

Integrated Analysis of Thermal/Structural/Optical Systems
B. Cullimore, T. Panczak, J. Baumann, Cullimore & Ring Technologies, Inc.
Dr. Victor Genberg,Sigmadyne Inc.
Mark Kahan, Optical Research Associates, Inc.


Automated Multidisciplinary Optimization of a Space-based Telescope
B. Cullimore, T. Panczak, J. Baumann, Cullimore & Ring Technologies, Inc.
Dr. Victor Genberg,Sigmadyne Inc.
Mark Kahan, Optical Research Associates, Inc

Further Data Exchange Standardization for Space Thermal Analysis
Hans Peter de Koning, ESA/ESTEC

 

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