Land-gear design and development testingThe X-15 airplane performance and operational requirements define a landing-gear system that will be subjected to high temperatures and high landing speeds and that will expend a minimum of airplane space and weight. This paper is concerned primarily with the landing-gear design configuration concept, the reporting of several unique design features that were incorporated, and description of the developmental testing of the subject system. (author)
Document ID
19930092405
Acquisition Source
Legacy CDMS
Document Type
None
Authors
Rhodes, L L
Date Acquired
August 15, 2013
Publication Date
July 30, 1958
Accession Number
93R21695
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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Related Records
IDRelationTitle19930092380Collected WorksResearch-Airplane-Committee Report on Conference on the Progress of the X-15 Project : A Compilation of the Papers Presented