Multi-Fidelity Design of an Integrated Thermal Protection System for Spacecraft Reentry
49th, Structures, structural dynamics and materials conference ; 2008 ; Schaumburg, IL
2008-01-01
13 pages
Aufsatz (Konferenz)
Englisch
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Comparison of Materials for an Integrated Thermal Protection System for Spacecraft Reentry
Online Contents | 2009
|INTEGRATED NON-REENTRY MANNED SPACECRAFT HULL DESIGN
AIAA | 1964
|