Start Date

4-1971 8:00 AM

Description

An analysis and status report of Space Shuttle booster configuration design features is presented. In comparing stowed, fixed straight, and "delta" wing basic configurations; the "delta" wing approach with a canard has been selected. Wing planform shape and cross-section is strongly influenced by air breathing engine installation requirements rather than purely aerodynamic performance optimization.

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Apr 1st, 8:00 AM

The Space Shuttle Booster

An analysis and status report of Space Shuttle booster configuration design features is presented. In comparing stowed, fixed straight, and "delta" wing basic configurations; the "delta" wing approach with a canard has been selected. Wing planform shape and cross-section is strongly influenced by air breathing engine installation requirements rather than purely aerodynamic performance optimization.

 

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