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
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.Download