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Environmental parameters of shuttle support for life sciences experimentsThe environments provided by the Orbiter vehicle and by the Spacelab will differ substantially from the environment provided by prior spacecraft. The specific design limits for each environmental parameter and expected operating characteristics are presented for both the Orbiter and the Spacelab. The environments are compared with those of earlier spacecraft and with the normal earth laboratory. Differences between the spacecraft environments and the normal laboratory environment and the impact of these differences on experiments and equipment design are discussed.
Document ID
19770036622
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Waligora, J. M.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1976
Subject Category
Man/System Technology And Life Support
Report/Patent Number
ASME PAPER 76-ENAS-24
Meeting Information
Meeting: Intersociety Conference on Environmental Systems
Location: San Diego, CA
Start Date: July 12, 1976
End Date: July 15, 1976
Sponsors: American Society of Mechanical Engineers
Accession Number
77A19474
Distribution Limits
Public
Copyright
Other

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