Thermal Results
All temperatures in C. Click on any image for a larger view.
PATRAN Thermal Images
with XN70/954-3 material
Predictions for half of array in direct sun
Beta 60 orbit, 12 minutes (first hot case)
Beta 60 orbit, 35 minutes (second hot case)
Beta 60 orbit, 58 minutes (first cold case)
Beta 60 orbit, 70 minutes (second cold case)
Beta 90 orbit, 12 minutes
Predictions for half of array shaded by spacecraft
Beta 60 orbit, 12 minutes (first hot case)
Beta 60 orbit, 35 minutes (second hot case)
Beta 60 orbit, 58 minutes (first cold case)
Beta 60 orbit, 75 minutes (second cold case)
Beta 90 orbit, 12 minutes
with M55J/954-3 material
Predictions for half of array in direct sun
Beta 60 orbit, 12 minutes (hot case)
Beta 60 orbit, 58 minutes (cold case)
Beta 90 orbit, 12 minutes
Predictions for half of array shaded by spacecraft
Beta 60 orbit, 12 minutes (hot case)
Beta 60 orbit, 58 minutes (cold case)
Beta 90 orbit, 12 minutes
Excel Plots
Beta 60 orbit transient
Beta 90 orbit transient
Return to STAR main page
Content Last Updated: April 12, 1999
By: r.m.amundsen@larc.nasa.gov
Site last reviewed: April 20, 2009.
Responsible NASA Official: Ruth M. Amundsen, Structural and Thermal Systems Branch, Systems Engineering Directorate,
Ruth.M.Amundsen@nasa.gov, (757) 864-7044
Site Curator: Ruth M. Amundsen, Structural and Thermal Systems Branch, Systems Engineering Directorate,
Ruth.M.Amundsen@nasa.gov, (757) 864-7044
Privacy Statement
Feedback on Langley Products and Services