Multidisciplinary Design Optimization of a Re-Entry Vehicle Shape and Trajectory
International conference; 10th, Space planes and hypersonic systems and technologies ; 2001 ; Kyoto, Japan
01.01.2001
9 pages
Contains papers AIAA-2001-1750 to 1927 only with gaps
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Coupled Shape and Reentry Trajectory Optimization of Entry Vehicle for Lunar Return
Tema Archiv | 2012
|