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Attitude controls for VTOL aircraftSystems consist of single duct system with two sets of reaction control nozzles, one linked mechanically to pilot's controls, and other set driven by electric servomotors commanded by preselected combinations of electrical signals.
Document ID
19710000201
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Pauli, F. A.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Subject Category
Life Sciences
Report/Patent Number
XAC-8972
Report Number: XAC-8972
Accession Number
71B10202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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