Study shows weight comparison or trend data between different vehicles and heat protection schemes; application is to lifting and ballistic-type entry vehicles undertaking satellite and circumlunar missions; structural cooling methods examined include radiation, ablation, and combinations of these methods.
Parametric weight study of manned space entry vehicle
Aerospace Eng
Aerospace Engineering ; 19 , n 10 ; p 40-49 + 77
1960
Aufsatz (Zeitschrift)
Englisch
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