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Flight demonstration of a nose-mounted rotating-solid-propellant rocket control system and a comparison with analog studiesFlight test of nose mounted rotating solid propellant rocket attitude control system for space vehicle second stage
Document ID
19660011640
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
James, R. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Williams, K. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3335
Report Number: NASA-TN-D-3335
Accession Number
66N20929
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATTITUDE CONTROL
SPACE VEHICLE CONTROL
SOLID PROPELLANT ROCKET ENGINE
FLIGHT TEST
SECOND STAGE

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