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Evaluation of the use of powered flight tracking and telemetry data in lunar orbit differential correction proceduresPowered flight maneuver data used to reduce state vector uncertainties for lunar satellite orbit differential correction
Document ID
19660016266
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lewis, D. H.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Communications
Report/Patent Number
NASA-CR-66064
Report Number: NASA-CR-66064
Accession Number
66N25555
Funding Number(s)
CONTRACT_GRANT: NAS1-4605-3
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT MANEUVER
LUNAR SATELLITE
ORBIT CALCULATION
STATE VECTOR
FLIGHT PATH
SATELLITE ORBIT

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