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Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase
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English
Abstract
An overview of Space Station Freedom Thermal Control System (TCS) and Environmental Control and Life Support System (ECLSS) integration is presented for Stages 2-6. Particular attention is given to issues associated with integrating five distinct, functioning spacecraft with hardware not specifically designed for intermediate stages. Areas specifically addressed include integrated ECLSS temperature and humidity control performance, thermal load balancing, performance and verification requirements, interface verification procedures, TCS activation sequence, resource allocation and Space Shuttle integration.
Authors
Citation
Di Pietro, D. and Tandler, J., "Integration of Thermal and Environmental Control Systems During Space Station Freedom Early Assembly Phase," SAE Technical Paper 921259, 1992, https://doi.org/10.4271/921259.Also In
References
- “Stage Data Book, Stage 6 Design and Performance” SSC 18010, Grumman Space Station Division 18 September 1991
- “Environmental Control and Life Support Systems Temperature and Humidity Control System Description Man-Tended Configuration” Boeing Defense and Space Group MSFC WP-1 Document No. D683-15005-1 18 October 1991
- “Environmental Control and Life Support Systems Atmosphere Control and Supply System Description Man-Tended Configuration” Boeing Defense and Space Group MSFC WP-1 Document No. D683-15007-1 18 October 1991
- “Environmental Control and Life Support Systems Atmosphere Revitalization System Description Man-Tended Configuration” Boeing Defense and Space Group MSFC WP-1 Document No. D683-15003-1 18 October 1991
- “Thermal Control System Man-Tended Configuration Preliminary Design Review” Boeing Defense and Space Group MSFC WP-1 Document No. D683-40102-1
- “Thermal Control System Architectural Control Document” NASA SSP 30258, MTC Addendum (Stage 6) 20 March 1992
- “Data Management System Architectural Control Document” NASA SSP 30261, Rev. D, Section 3 September 1991
- “Assembly Operations and Engineering Assessment” NASA SSJ 10310 Johnson Space Center September 1991
- “External Active Thermal Control System Flight System Software Requirements Presentation for TWG 12” Monheit M. LESC, Space Station Freedom Thermal Control System Working Group #12, Johnson Space Center 25-28 February 1992
- “Integrated Operational Scenarios, MB-1 through MB-7, and UF-1” JSC 36024 Johnson Space Center February 1992
- “Thermal Control System Flight System Software Requirements Document” II External Thermal Control System, NASA SSJ 10430 27 February 1992
- “WP-02 Thermal Control System Activation, External and Internal Thermal Control System” Kosyk K. MDSSC, Space Station Freedom Thermal Control System Working Group #12 Johnson Space Center 25-28 February 1992
- “ITCS FSSR Presentation for TWG 12” Engeset M. Boeing Defense and Space Group, Space Station Freedom Thermal Control System Working Group #12 Johnson Space Center 25-28 February 1992
- “Environmental Control and Life Support System Architectural Control Document” Rev. D, NASA SSP 30262 15 July 1991
- “Space Station Program Definition and Requirements, Section 6: Resource Allocation” NASA SSP 30000, Section 6, Rev. F June 1991