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Entry capsule orbit determination accuracyOn-board tracking system of two-way coherent Doppler between entry capsule and orbiting bus for determining orbit of entry capsule and estimating atmospheric parameters.
Document ID
19670006575
Acquisition Source
Jet Propulsion Laboratory
Document Type
Contribution to a larger work
Authors
C. Scranage (Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
August 3, 2013
Publication Date
November 30, 1966
Publication Information
Publication: Space Programs Summary 37-42 The Deep Space Network for the Period September 1 to October October 31, 1966
Publisher: Jet Propulsion Lab
Volume: 3
Issue Publication Date: November 30, 1966
Subject Category
Space Sciences
Report/Patent Number
N67-15904
Accession Number
67N15904
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
COHERENT RADAR
MARS ATMOSPHERE
SPACE BUS
TRACKING SYSTEM
CAPSULE
ORBIT CALCULATION
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