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MIL-D-19326 Revision H:1990
Current
The latest, up-to-date edition.
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Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for
31-08-1990
Details requirements for the design and installation of liquid oxygen 70 and 300 psig (483 kPa and 2068 kPa) systems in aircraft.
DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
DocumentType |
Standard
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Pages |
69
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Current
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This specification covers the general requirements for the design and installation of liquid oxygen (70 and 300 pounds per square inch gauge) (psig) (483KPa and 2068 kPa) systems in aircraft.
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