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Orbiter active thermal control system descriptionA brief description of the Orbiter Active Thermal Control System (ATCS) including (1) major functional requirements of heat load, temperature control and heat sink utilization, (2) the overall system arrangement, and (3) detailed description of the elements of the ATCS.
Document ID
19750056783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Laubach, G. E. (Rockwell International Corp. Space Div., Downey, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1975
Subject Category
Man/System Technology And Life Support
Report/Patent Number
ASME PAPER 75-ENAS-58
Meeting Information
Meeting: Intersociety Conference on Environmental Systems
Location: San Francisco, CA
Start Date: July 21, 1975
End Date: July 24, 1975
Sponsors: AIAA, ASME, SAE, ASMA, AIChE
Accession Number
75A40855
Funding Number(s)
CONTRACT_GRANT: NAS9-14000
Distribution Limits
Public
Copyright
Other

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