The purpose of this report is to document progress to date on the structural design effort conducted by the Preliminary Design Group, Advanced Structures Branch, Structures Division, in support of a Prototype Division VISTOL Aircraft. The investigation of the use of the Cold Thrust Augmentation (CTA) principle on a VISTOL aircraft was limited to two Prototype Division generated configurations. One configuration involved a CTA pod located at the wing tip while the second configuration was a fuselage mounted CTA system.
Structural Design Considerations for Cold Thrust Augmentation Fighter Concepts
1973
29 pages
Report
Keine Angabe
Englisch
Design considerations in the use of solid motors for thrust augmentation
Tema Archiv | 1975
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