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A LOOK AT MANNED ENTRY AT CIRCULAR TO HYPERBOLIC VELOCITIESManned space vehicle reentry at circular to hyperbolic velocities, considering deceleration, corridor width, heating, heat protection, vehicle weight, lateral ranging, and landing factors
Document ID
19630022945
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Love, E. S.
Pritchard, E. B.
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Space Radiation
Accession Number
63A19004
Distribution Limits
Public
Copyright
Other
Keywords
REENTRY CONDITION
SPACECRAFT REENTRY
MANNED SPACECRAFT

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