Preliminary Design of the Space Station Internal Thermal Control System Systems Analysis and Integration Lab., NASA/Marshall Space Flight Center, AL

Format:

Conference/Event

Author/Creator:

Herrin, Mark T., author.

Conference Name:

Intersociety Conference on Environmental Systems (1987-07-13 : Seattle, Washington, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1987

Summary:

The baseline preliminary design configuration of the Internal Thermal Control System (ITCS) of the United States (U.S.) Space Station (SS) pressurized elements (id est, the Habitation and U.S. Laboratory modules, pressurized logistics carrier, and resources nodes) is defined. The ITCS is composed of both active and passive components. The subsystems which comprise the ITCS are identified and their functional descriptions are provided. The significant trades and analyses, which were performed during Phase B (id est, the preliminary design phase) that resulted in the design described herein, are discussed. The ITCS interfaces with the station's central Heat Rejection and Transport System (HRTS), other systems, and externally attached pressurized payloads are described. Requirements on the ITCS with regard to redundancy and experiment support are also addressed

Notes:

Vendor supplied data

Publisher Number:

871505

Access Restriction:

Restricted for use by site license