Design and fabrication of a titanium matrix composite (TMC) F-15 nose landing gear (NLG) outer cylinder is discussed. Results of a field experience survey examining landing gear (LG) operations are also discussed. Weight, supportabilty and cost benefits are summarized for this component and projected for production applications of the material.
Titanium Matrix Composite Landing Gear Development
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1989
1989-09-01
Aufsatz (Konferenz)
Englisch
Titanium matrix composite landing gear development
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