An Investigation of Leakage of Large-diameter O-ring Seals on Spacecraft Air-lock Hatches PDF Download
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Author: Otto F. Trout
Publisher:
ISBN:
Category : O-rings
Languages : en
Pages : 44
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Book Description
Author: Otto F. Trout
Publisher:
ISBN:
Category : O-rings
Languages : en
Pages : 44
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Book Description
Author: Otto F. Trout
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
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Book Description
Author: Otto F. Trout
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Author: Otto F. Trout (Jr.)
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 50
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Book Description
A lightweight simulated spacecraft air-lock structure was tested under high vacuum to evaluate structural sealing problems and to determine leakage rates. Three different types of hatch configurations and three different seal configurations were tested for a temperature range of from -40° F (-40° C) to 200' F (930 C). Leakage rates of less than 1 x cc/sec or less than 10 (to the power of negative 4) cc/day of helium (standard temperature and pressure) were attained for each hatch.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 700
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 472
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 472
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1498
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
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Book Description
