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Thermal Design of Space Support Equipment for the Hubble Space Telescope Servicing Mission
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English
Abstract
During the First Servicing Mission for the Hubble Space Telescope, two replacement instruments and several spacecraft components were installed successfully. Most of the replacement hardware was carried up in protective enclosures that provided thermal control over a wide range of potential mission attitudes. Some items added late to the mission were protected by passive thermal systems and attitude constraints on the Shuttle. This paper focuses on thermal design challenges presented by the replacement hardware, enclosures, and carriers, and includes an assessment of flight thermal performance.
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Citation
Ousley, W., "Thermal Design of Space Support Equipment for the Hubble Space Telescope Servicing Mission," SAE Technical Paper 941571, 1994, https://doi.org/10.4271/941571.Also In
References
- Davis, A. HST Servicing Mission Space Support Equipment Thermal Analysis Report May 1993
- Davis, A. Parrish, K. Update to HST Servicing Mission Space Support Equipment Thermal Analysis November 1993
- Krein, S. BISIPE Thermal Balance Test Report June 1993
- Harris, D. Thermal Analysis Results for SADE Transistors August 1993
- Krein, S. Axial SIPE Lid Closure Thermal Test Report January 1993
- Niedringhaus, W. HST First Servicing Mission Correlation Status February 1994