Feasibility of utilizing nozzle separation as method of thrust vector control is discussed; preceding work was mainly study and analysis of nozzle separation; these results are applied to guidance problem; possibility of using nozzle separation as method for thrust vector control is dealt with; guidance problem is reviewed and trend toward purely aerodynamic vectoring through secondary injection is discussed; nozzle separation approach is broken into two areas -- controllability and magnitude; tests in these areas indicate that nozzle separation can be controlled and is of adequate magnitude to complement secondary injection as means of thrust vectoring. (22915)
Controlled nozzle separation for thrust vectoring
AIAA Student J
AIAA Student Journal ; 6 , n 3
1968
4 pages
Aufsatz (Zeitschrift)
Englisch
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