Space shuttle design verification requires dynamic data from full scale structural component and assembly tests. Wind tunnel and other scaled model tests are also required early in the development program to support the analytical models used in design verification. Presented is a design philosophy based on mathematical modeling of the structural system strongly supported by a comprehensive test program; some of the types of required tests are outlined.
Dynamic testing for shuttle design verification
01.07.1972
Aufsatz (Konferenz)
Keine Angabe
Englisch
Dynamic analysis for shuttle design verification
NTRS | 1972
|Design verification testing of space shuttle main engine transducers
Tema Archiv | 1978
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