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High-speed T-38A landing gear extension loadsTesting of T-38A landing gear extension at high speed and high altitude is described. The mechanisms are shown together with peak hydraulic pressure data during landing gear deployment with active and inactive strut door flaps. Results of strain gage measurements of stress on various structural members are included.
Document ID
19800016824
Document Type
Technical Memorandum (TM)
Authors
Schmitt, A. L. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1980
Subject Category
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Report/Patent Number
NASA-TM-58226
JSC-16497
Funding Number(s)
PROJECT: RTOP 953-36-00-00-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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