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Integrated Energy Balance Analysis for Space Station Freedom

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Tandler, John, author.
Conference Name:
International Conference On Environmental Systems (1991-07-08 : San Francisco, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1991
Summary:
An integrated simulation model is described which characterizes the dynamic interaction of the energy transport subsystems of Space Station Freedom for given orbital conditions and for a given set of power and thermal loads. Subsystems included in the model are the Electric Power System (EPS), the Internal Thermal Control System (ITCS), the External Thermal Control System (ETCS), and the cabin Temperature and Humidity Control System (THC) (which includes the avionics air cooling, cabin air cooling, and inter-module ventilation systems). Models of the subsystems were developed in a number of system-specific modeling tools and validated. The subsystem models are then combined into integrated models to address a number of integrated performance issues involving the ability of the integrated energy transport system of Space Station Freedom to provide power, controlled cabin temperature and humidity, and equipment thermal control to support operations
Notes:
Vendor supplied data
Publisher Number:
911338
Access Restriction:
Restricted for use by site license

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