NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Spin-rate control deviceInnovation eliminates need for driver, sensor, and interconnecting logic circuits. Device combines simplicity of fixed-fin concept with precise rate control provided by active flight control system.
Document ID
19760000417
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Nolte, L. J.
(Hughes Aircraft Co.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-10884
Report Number: ARC-10884
ISSN: 0145-319X
Accession Number
76B10417
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available