Constructing a Spatial Attainability Region for a Spacecraft Entering the Atmosphere with Near-Circular Velocity and a Large Entry Angle

Details Constructing a Spatial Attainability Region for a Spacecraft Entering the Atmosphere with Near-Circular Velocity and a Large Entry Angle Constructing a Spatial Attainability Region for a Spacecraft Entering the Atmosphere with Near-Circular Velocity and a Large Entry Angle

Jan 1996

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1996cosre..34...75k&link_type=openurl

Cosmic Research, Vol. 34, No. 1, p.75

Physics

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