Functional relations are developed for ablation, insulation, and structural weights for ballistic-type entry vehicles as functions of vehicle and atmospheric properties; by application of these relations to range of possible model atmospheres for Mars, effects of these uncertainties on vehicle design weights and sizes are determined.
Effects of Mars atmospheric uncertainties on entry vehicle design
Aerospace Eng
Aerospace Engineering ; 21 , n 12
1962
5 pages
Aufsatz (Zeitschrift)
Englisch
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