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Correlation of angle-of-attack envelopes for spinning entry bodies.Relation between angle of attack envelopes and correlation parameter for spinning bodies entering atmosphere at large inclinations
Document ID
19660033521
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Peterson, V. L.
Tobak, M.
Date Acquired
August 3, 2013
Publication Date
November 1, 1965
Subject Category
Space Vehicles
Accession Number
66A12811
Distribution Limits
Public
Copyright
Other
Keywords
ANGLE OF ATTACK
REENTRY BODY
CORRELATION COEFFICIENT
SPIN DYNAMICS

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