MIL-D-19326 Revision H:1990
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Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for
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31-08-1990
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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
|
| Pages |
69
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
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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