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The influence of oscillator instability on orbit accuracyInfluence of Doppler tracking system oscillator instability on orbit accuracy
Document ID
19670005100
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Curkendall, D. W. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
September 30, 1966
Subject Category
Communications
Accession Number
67N14429
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
OSCILLATOR
DOPPLER RADAR
TRACKING SYSTEM
ORBIT CALCULATION
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