Short Courses

Thermal Vacuum Testing
Thursday, August 21, 2003
8:00 AM to 12:00 PM

Carol Mosier (GSFC)
(301) 286-3168
Carol.L.Mosier@nasa.gov

Glenn Tsuyuki (JPL)
(818) 354-2955
Glenn.T.Tsuyuki@jpl.nasa.gov


This course will include lectures on best practices, test preparation, and testing methods in the field of thermal vacuum testing, an important element of the integration and testing of a spacecraft. It will include presentations from both NASA's Jet Propulsion Laboratory and NASA Goddard Space Flight Center. This course is taught starting from the basics and will end with discussion on the differences between methods employed by these two NASA facilities, as well as input from the audience. See also Thermal Vacuum Testing Panel Meeting.


CFD-Thermal Integration for Aeroheating Problems
Thursday, August 21, 2003
1:30 PM to 5:30 PM

Dr. Kim Bey (NASA LaRC)
(757) 864-1351
Kim.S.Bey@nasa.gov

Frank Milos (NASA ARC)
(650) 604-5636
fmilos@mail.arc.nasa.gov

Gerald Russell, PhD, (U.S. Army)
(256) 876-1712
Gerald.Russell@rdec.redstone.army.mil

This course will include presentations from NASA Langley Research Center, NASA Ames Research Center, and DOD/US Army and will discuss the state-of-the-art in the integration of CFD and thermal analysis specifically in the area of aeroheating analysis. Individual presentations will be approximately 1 hour and there will also be time for discussion on methods and techniques. The idea of this short course is to bring together experts in different techniques for performing aeroheating analysis to promote an understanding of the differences and to open up discussion on which techniques apply best to certain aeroheating situations

An overview of the process and critical issues associated with aerothermal analysis and design of supersonic and hypersonic systems will be presented. Topics will include analysis and design tools, development of aerothermal boundary conditions using engineering methods and the applicability of computational fluid dynamics, thermal protection system predictive models, and airframe/internal component thermal management. An example of the development of a hypersonic heatshield application will be provided to demonstrate the analysis and design process.


Thermal Control Hardware
Friday, August 22, 2003
8:00 AM to 12:00 PM

Donya Douglas (Thermal Surfaces)
(301) 286-6952
Donya.M.Douglas@nasa.gov

Dr. Jehntung Ku (2 Phase Flow Heat Transfer)
(301) 286-3130
Jentung.Ku-1@nasa.gov

Paul Whitehouse
(301) 286-8378
Paul.Whitehouse@gsfc.nasa.gov

Max Blosser (Metallic TPS)
(757) 864-5192
Max.L.Blosser@nasa.gov


This course will focus on 4 distinct areas of thermal control. An expert in each area will present for 45 minutes, and an hour will be devoted to a panel question and answer session at the end of the course. The four areas that were chosen for this year's course are:

  • Thermal Surface Technology (variable emittance coatings, MEMS louvers, electrochromics, electrostatic flaps)
  • 2 Phase Flow Heat Transfer Technology (heat pipes, CPLs, loop heat pipes)
  • Cyrogenic Technology (cryogens, cryostats, cryocoolers, tactical coolers)
  • Metallic TPS Technology