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Steady-state characteristics of a differential -pressure system for evaluating angles of attack and sideslip of the ranger iv vehicleSteady-state characteristics of differential pressure system for evaluating angles of attack and sideslip of ranger iv vehicle
Document ID
19640000610
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fox, A. G. (NASA Langley Research Center Hampton, VA, United States)
Yates, E. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1966
Report Number: NASA-TN-D-1966
Accession Number
64N10519
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STEADY STATE
PRESSURE
ANGLE OF ATTACK
SIDESLIP
RANGER IV LUNAR PROBE

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