Tests at Langley landing-loads track to obtain friction coefficients developed during braking and landing were made at forward speeds of 85 knots with static vertical loads of 20,405 and 13,020 lb; results indicated effect of each type of mat and membrane on variation of coefficient of friction; braking tests for both dry and wet surface conditions.
Braking and landing tests on some new types of airplane landing mats and membranes
NASA -- Tech Note
1959
41 pages
Report
English
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Development of airplane landing mats
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