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A Representative Shuttle Environmental Control SystemThe Representative Shuttle Environmental Control System (RSECS) provides a ground test bed to be used in the early accumulation of component and system operating data, the evaluation of potential system improvements, and possibly the analysis of Shuttle Orbiter test and flight anomalies. Selected components are being subjected to long term tests to determine endurance and corrosion resistance capability prior to Orbiter vehicle experience. Component and system level tests in several cases are being used to support flight certification of Orbiter hardware. These activities are conducted as a development program to allow for timeliness, flexibility, and cost effectiveness not possible in a program burdened by flight documentation and monitoring constraints.
Document ID
19770064014
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brose, H. F.
(Hamilton Standard Windsor Locks, CT, United States)
Stanley, M. D.
(United Technologies Corp. Hamilton Standard Div., Windsor Locks, Conn., United States)
Leblanc, J. C.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1977
Subject Category
Man/System Technology And Life Support
Report/Patent Number
ASME PAPER 77-ENAS-25
Meeting Information
Meeting: Intersociety Conference on Environmental Systems
Location: San Francisco, CA
Country: US
Start Date: July 11, 1977
End Date: July 14, 1977
Sponsors: SAE, ASME, AIAA, AIChE, ASMA
Accession Number
77A46866
Distribution Limits
Public
Copyright
Other

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