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Improved aircraft reaction nozzlesReaction control nozzle requires low operating forces and has linear and predictable jet thrust vs nozzle exit area and position. Nozzle thrust vector is controllable by single rotary motion.
Document ID
19750000284
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Rogers, J. R.
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Subject Category
Mechanics
Report/Patent Number
ARC-10906
Accession Number
75B10284
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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