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Effect of target angular oscillations on pilot-controlled Gemini-Agena dockingTarget angular oscillation effects on pilot- controlled Gemini-Agena docking
Document ID
19660013632
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cobb, J. B. (NASA Langley Research Center Hampton, VA, United States)
Jaquet, B. M. (NASA Langley Research Center Hampton, VA, United States)
Riley, D. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-3403
Report Number: NASA-TN-D-3403
Accession Number
66N22921
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
OSCILLATION
GEMINI SPACECRAFT
AGENA ROCKET
DOCKING
ANGULAR MOTION

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