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A supercircular entry guidance concept designed for maximum monitoring capabilityReentry vehicle guidance system for automatic or manual range control and with pilot monitoring capability
Document ID
19660028392
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Havill, C. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Stinnett, G. W.
(NASA Ames Research Center Moffett Field, CA, United States)
White, K. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Navigation
Report/Patent Number
NASA-TN-D-3668
Report Number: NASA-TN-D-3668
Accession Number
66N37682
Funding Number(s)
CONTRACT_GRANT: 125-17-05-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GUIDANCE SYSTEM
REENTRY VEHICLE
RANGE CONTROL
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