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Maneuvering flight within earth-entry corridors at hyperbolic speeds.Reentry flight corridor depth reduction as result of inadequate flight data at hyperbolic speeds, noting overshoot limit and inverted attitude
Document ID
19650032301
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlson, R. W.
Swenson, B. L.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 65-19
Report Number: AIAA PAPER 65-19
Accession Number
65A15005
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT MANEUVER
GEOMAGNETICALLY TRAPPED PARTICLE
PITCH CONTROL
HYPERBOLIC REENTRY
REENTRY TRAJECTORY
ADIABATIC EQUATION

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