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Experimental evaluation of the Skylab orbital workshop ventilation system conceptExtensive testing was conducted to evaluate the Orbital Workshop ventilation concept. Component tests were utilized to determine the relationship between operating characteristics at 1 and 0.34 atm. System tests were conducted at 1 atm within the Orbital Workshop full-scale mockup to assess delivered volumetric flow rate and compartment air velocities. Component tests with the Anemostat circular diffusers (plenum- and duct-mounted) demonstrated that the diffuser produced essentially equivalent airflow patterns and velocities in 1- and 0.34-atm environments. The tests also showed that the pressure drop across the diffuser could be scaled from 1 to 0.34 atm using the atmosphere pressure ratio. Fan tests indicated that the performance of a multiple, parallel-mounted fan cluster could be predicted by summing the single-fan flow rates at a given delta P.
Document ID
19730008148
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Allums, S. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hastings, L. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Ralston, J. T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
March 14, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-64700
Report Number: NASA-TM-X-64700
Accession Number
73N16875
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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