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Centrifugal simulation of the X-15Paper presents the results of physiological tolerance tests of the pilot to the oscillating accelerations of large amplitude and long duration which might occur as a result of aircraft heading errors during reentries from the altitude mission in the X-15 without control augmentation.
Document ID
19930092388
Acquisition Source
Legacy CDMS
Document Type
None
Authors
Clark, Carl
Date Acquired
August 15, 2013
Publication Date
July 30, 1958
Accession Number
93R21678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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