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Explicit guidance equations for multistage boost trajectoriesExplicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajectory
Document ID
19660006073
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Teren, F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-3189
Accession Number
66N15362
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MULTISTAGE VEHICLE
SPACECRAFT GUIDANCE
ATLAS CENTAUR LAUNCH VEHICLE
STEERING
TRAJECTORY OPTIMIZATION
LUNAR TRAJECTORY

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