An assessment of habitat pressure, oxygen fraction, and EVA suit design for space operations

At high cabin pressure [e.g. 1013 hPa (14.7 psi) 21% O 2] there are serious issues relative to specification of suit pressure and the need for prebreathing. A high pressure suit will be costly but use of the existing, flexible suit requires up to 6 h of prebreathing. Or one could use a cabin pressur...

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Published inActa astronautica Vol. 32; no. 1; pp. 39 - 49
Main Authors Morgenthaler, George W., Fester, Dale A., Cooley, Carolyn G.
Format Journal Article
LanguageEnglish
Published England Elsevier Ltd 1994
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Abstract At high cabin pressure [e.g. 1013 hPa (14.7 psi) 21% O 2] there are serious issues relative to specification of suit pressure and the need for prebreathing. A high pressure suit will be costly but use of the existing, flexible suit requires up to 6 h of prebreathing. Or one could use a cabin pressure of 700 hPa (10.2 psi) prior to extravehicular activity (EVA) in order to use the existing suit with only 1 h of prebreathing. If these normal cabin pressures and O 2 levels are utilized, existing physiological and medical databases apply, providing a known basis for evaluating effects of long duration space missions. If a 345 hPa (5 psi), 70–100% O 2 atmosphere is adopted the existing suit can be used with no prebreathing required. However, there is no reference database on physiological effects under the conditions of lower pressure and higher O 2 concentration. This paper considers the major issues involved in defining habitat pressure, O 2 fraction, and EVA suit design for operations in space. A preliminary model for evaluating habitat/suit pressure and O 2% strategies is presented.
AbstractList At high cabin pressure [e.g. 1013 hPa (14.7 psi) 21% O 2] there are serious issues relative to specification of suit pressure and the need for prebreathing. A high pressure suit will be costly but use of the existing, flexible suit requires up to 6 h of prebreathing. Or one could use a cabin pressure of 700 hPa (10.2 psi) prior to extravehicular activity (EVA) in order to use the existing suit with only 1 h of prebreathing. If these normal cabin pressures and O 2 levels are utilized, existing physiological and medical databases apply, providing a known basis for evaluating effects of long duration space missions. If a 345 hPa (5 psi), 70–100% O 2 atmosphere is adopted the existing suit can be used with no prebreathing required. However, there is no reference database on physiological effects under the conditions of lower pressure and higher O 2 concentration. This paper considers the major issues involved in defining habitat pressure, O 2 fraction, and EVA suit design for operations in space. A preliminary model for evaluating habitat/suit pressure and O 2% strategies is presented.
At high cabin pressure, there are serious issues relative to specification of suit pressure and the need for prebreathing. A high pressure suit will be costly but the use of the existing flexible suit requires up to 6 h of prebreathing. If normal cabin pressures and O2 levels are utilized, existing physiological and medical databases apply, providing a known basis for evaluating effects of long duration space missions. If a 5 psi, 70-100 percent O2 atmosphere is adopted, the existing suit can be used with no prebreathing required. However, there is no reference database on physiological effects under the conditions of lower pressure and higher O2 concentration. This paper considers the major issues involved in defining habitat pressure, O2 fraction, and EVA suit design for operations in space. A preliminary model for evaluating habitat/suit pressure and O2 percent strategies is presented.
At high cabin pressure [e.g. 1013 hPa (14.7 psi) 21% O2] there are serious issues relative to specification of suit pressure and the need for prebreathing. A high pressure suit will be costly but use of the existing, flexible suit requires up to 6 h of prebreathing. Or one could use a cabin pressure of 700 hPa (10.2 psi) prior to extravehicular activity (EVA) in order to use the existing suit with only 1 h of prebreathing. If these normal cabin pressures and O2 levels are utilized, existing physiological and medical databases apply, providing a known basis for evaluating effects of long duration space missions. If a 345 hPa (5 psi), 70-100% O2 atmosphere is adopted the existing suit can be used with no prebreathing required. However, there is no reference database on physiological effects under the conditions of lower pressure and higher O2 concentration. This paper considers the major issues involved in defining habitat pressure, O2 fraction, and EVA suit design for operations in space. A preliminary model for evaluating habitat/suit pressure and O2% strategies is presented.
Author Cooley, Carolyn G.
Morgenthaler, George W.
Fester, Dale A.
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References Space Station Freedom Data Package, received from Dr Richard Keefe, NASA Headquarters. This data is a compendium of information compiled by Dr Keefe during the SSF program evaluation of cabin and suit pressures. It was not always apparent as to who was the actual author of the material. For acknowledgement purposes, the entire package is referenced in this paper. Where possible, known sources are referenced.
Assessment of Technologies for the Space Exploration Initiative (SEI) (BIB3) 1990
Gell (BIB5) 1962; 33
(BIB1) 1964
Fuller (BIB6) 1985
Parker (BIB4) 1964
McDonnell Douglas, EVA system and operations (Criteria). Contained in Ref. [2].
(10.1016/0094-5765(94)90146-5_BIB1) 1964
10.1016/0094-5765(94)90146-5_BIB2
Gell (10.1016/0094-5765(94)90146-5_BIB5) 1962; 33
Assessment of Technologies for the Space Exploration Initiative (SEI) (10.1016/0094-5765(94)90146-5_BIB3) 1990
10.1016/0094-5765(94)90146-5_BIB7
Fuller (10.1016/0094-5765(94)90146-5_BIB6) 1985
Parker (10.1016/0094-5765(94)90146-5_BIB4) 1964
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  publication-title: Bioastronautics Data Book
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  article-title: The space station atmosphere (draft)
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  article-title: Biological effects of simulated micrometeoroid penetration of a sealed chamber containing animal specimens
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Snippet At high cabin pressure [e.g. 1013 hPa (14.7 psi) 21% O 2] there are serious issues relative to specification of suit pressure and the need for prebreathing. A...
At high cabin pressure [e.g. 1013 hPa (14.7 psi) 21% O2] there are serious issues relative to specification of suit pressure and the need for prebreathing. A...
At high cabin pressure, there are serious issues relative to specification of suit pressure and the need for prebreathing. A high pressure suit will be costly...
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SubjectTerms Aerospace Medicine
Atmospheric Pressure
Equipment Design
Equipment Safety
Extravehicular Activity
Humans
Models, Theoretical
Oxygen - analysis
Oxygen Inhalation Therapy
Space Flight - economics
Space Flight - instrumentation
Space Flight - trends
Space life sciences
Space Suits
Spacecraft
Title An assessment of habitat pressure, oxygen fraction, and EVA suit design for space operations
URI https://dx.doi.org/10.1016/0094-5765(94)90146-5
https://www.ncbi.nlm.nih.gov/pubmed/11541018
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