Method of calculating trajectories of occupied seats or capsules ejected from aircraft flying at high speed provides preliminary analytical tool for evaluation of conditions required to prevent collision of objects with tail of aircraft; general solution of special case is given in which aerodynamic and rocket thrust coefficients are assumed to be constant; graphs of available results of wind-tunnel tests and example calculation.
Trajectories of objects ejected from aircraft
Can Aeronautical J
Canadian Aeronautical Journal ; 6 , n 1
1960
7 pages
Aufsatz (Zeitschrift)
Englisch
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