Application of NASTRAN to structural analysis of space shuttle orbiter finite element model with over 3000 joint degrees of freedom
Application of NASTRAN to the Analysis of a Space Shuttle Orbiter Structure
1971-09-01
Sonstige
Keine Angabe
Englisch
Application of NASTRAN to a Space Shuttle Dynamics Model
NTRS | 1971
|Space Shuttle Orbiter Barricade
NTIS | 1974
|Space shuttle orbiter avionics
Tema Archiv | 1977
|NTIS | 1994
NTRS | 1973
|