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Optimum deorbit positioning for minimum impulse reentry.Optimum deorbit positioning on planetocentric elliptic orbit for single impulse reentry treated by two coupled quartic polynomials
Document ID
19670048807
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stern, G. S.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Space Sciences
Report/Patent Number
AAS PAPER 66-123
Report Number: AAS PAPER 66-123
Accession Number
67A27536
Funding Number(s)
CONTRACT_GRANT: NAS9-4810
Distribution Limits
Public
Copyright
Other
Keywords
REENTRY PHYSICS
IMPULSE ORBITAL TRANSFER
ELLIPTICAL ORBIT
TRAJECTORY OPTIMIZATION

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