Run Time Improvement Efforts for the Roman Space Telescope Thermal Analysis

Date

7/12/2021

Journal Title

Journal ISSN

Volume Title

Publisher

50th International Conference on Environmental Systems

Abstract

Observatory thermal models for large, complex missions, such as the Roman Space Telescope (RST) produce an immense amount of data to be processed. RST is a large scale, flagship Astrophysics mission for NASA with challenging wave front error stability requirements and utilizes a single model for thermal discipline analysis and thermo-optical distortion analysis. In alleviating the need to maintain two models for different analysis types, it imposes run time penalties on the thermal analysis. Throughout the lifecycle of the project, the component models have steadily grown in size, resulting in a continuous growth of the overall observatory model with each update and a considerable increase in the model run time. While ongoing efforts to reduce run time are continuously investigated, previous efforts had primarily focused on timestep size and total simulation time to reach quasi-equilibrium. More recently, studies were performed on the total number of radiation couplings (radks) included in the model, which has a linear impact on run time, but increases exponentially with node count. As standard practice for spacecraft analysis, small radks were excluded from the temperature solution based on the assumption that their interchange/view factors have a negligible impact on heat flow. Four approaches were investigated to reduce the model run time while minimizing the impact on accuracy: Equivalent Radiation Network node, Progressive Radk Inclusion, Targeted Radk Filtering for critical/non critical areas, and Representation of culled radks with Backloads. Furthermore, the investigation of model run time also revealed that cold cases took noticeably longer to run than hot cases; the root computational inefficiencies were explored along with the computation penalty of linearization of the external radks and recalculation of temperature dependent linear couplings at each timestep. This paper outlines the details of each of the above approaches and their impact on run time and model accuracy.

Description

Hume Peabody, NASA
Eric Yee, NASA
ICES207: Thermal and Environmental Control Engineering Analysis and Software
The 50th International Conference on Environmental Systems was held virtually on 12 July 2021 through 14 July 2021.

Keywords

Thermal Analysis, Roman Space Telescope, Run Time

Citation