|
rdf:type |
|
|
lifeskim:mentions |
|
|
pubmed:issue |
1
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pubmed:dateCreated |
2002-9-5
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pubmed:abstractText |
To select the suitable material for the structure of simulated space cabin to meet the special requirements which the unitary metallic material cannot do.
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pubmed:language |
chi
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pubmed:journal |
|
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pubmed:citationSubset |
S
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pubmed:chemical |
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pubmed:status |
MEDLINE
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|
pubmed:month |
Feb
|
|
pubmed:issn |
1002-0837
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|
pubmed:author |
|
|
pubmed:issnType |
Print
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pubmed:volume |
13
|
|
pubmed:owner |
NASA
|
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pubmed:authorsComplete |
Y
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pubmed:pagination |
48-51
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pubmed:dateRevised |
2010-3-24
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pubmed:meshHeading |
pubmed-meshheading:12214611-Compressive Strength,
pubmed-meshheading:12214611-Elasticity,
pubmed-meshheading:12214611-Epoxy Compounds,
pubmed-meshheading:12214611-Facility Design and Construction,
pubmed-meshheading:12214611-Gases,
pubmed-meshheading:12214611-Glass,
pubmed-meshheading:12214611-Materials Testing,
pubmed-meshheading:12214611-Metals,
pubmed-meshheading:12214611-Plastics,
pubmed-meshheading:12214611-Space Simulation,
pubmed-meshheading:12214611-Spacecraft,
pubmed-meshheading:12214611-Stress, Mechanical,
pubmed-meshheading:12214611-Tensile Strength
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|
pubmed:year |
2000
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|
pubmed:articleTitle |
[Material selection and structural design of simulated space module for field].
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|
pubmed:affiliation |
Institute of Space Medico-Engineering, Beijing, China.
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|
pubmed:publicationType |
Journal Article,
Comparative Study,
English Abstract
|
