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Manual control of high-altitude Apollo launch abortSimulation study of manual control capability for Apollo spacecraft reentry orientation after high altitude launch abort using visual scene
Document ID
19660018746
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Driscoll, N. R. (NASA Langley Research Center Hampton, VA, United States)
Garren, K. R. (NASA Langley Research Center Hampton, VA, United States)
Meintel, A. J., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3433
Accession Number
66N28036
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REENTRY
MANUAL CONTROL
ATTITUDE CONTROL
SIMULATION
APOLLO SPACECRAFT
ABORT

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