Space Station Freedom main truss thermal analysis

Abstract

The main truss structure of the Permanently Manned Capability configuration of the Space Station Freedom is analyzed in order to evaluate orbital heating loads and determine the temperature distributions and temperature gradients in the structure. The results are to be utilized in a thermal/structure analysis in the determination of thermal stresses and deflections in the truss members caused by solar heating loads and by shadowing of the truss members by other segments of the Space Station as it moves around the orbit. A SINDA thermal finite different model and a TRASYS radiation interchange model of the truss were generated automatically from a NASTRAN finite element structural model. The analysis yielded transient temperature distribution in the truss structure around the orbit, indicating large temperature gradients in the structure.