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NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
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AA-CP-20212-001
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ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
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MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
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NASA-MEMO-12-20-58L

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  • May 10, 2017 Create Date
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Investigation of the Maximum Spin-Up Coefficients of Friction Obtained During Tests of a Landing Gear Having a Static Load Rating of 200,000 Pounds

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NASA-MEMO-12-20-58L

  • Version
  • 79 Downloads
  • 1.11 MB File Size
  • 1 File Count
  • May 10, 2017 Create Date
  • May 10, 2017 Last Updated
Scroll for Details

Investigation of the Maximum Spin-Up Coefficients of Friction Obtained During Tests of a Landing Gear Having a Static Load Rating of 200,000 Pounds

FileAction
NASA-MEMO-12-20-58L Investigation of the Maximum Spin-Up Coefficients of Friction Obtained During Tests of a Landing Gear Having a Static Load Rating of 200,000 Pounds.pdfDownload 
17,005 Documents in our Technical Library
2463489 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...