Criterion of comparison of aerodynamic layouts and selection of an aerodynamic configuration of reusable winged boosters perspective transport space systems

Space technics and technology


Аuthors

Chibisov Y. N.

JSC NPO Molniya,

e-mail: chibisovyan@bk.ru

Abstract

The research is conducted at the choice of an aerodynamic configuration of a reusable winged booster of transport space systems. The methodology (criterion) of comparison of aerodynamic layouts of boosters is designed. The aerodynamic layouts of a reusable winged booster executed on aerodynamic configurations "normal", "tailless", "canard" are designed. Their computational balancing aerodynamic performances are determined.


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