Expendable second stage reusable space shuttle booster. Volume 4: Detail mass properties data
nasa
Abstract
nasa
Abstract
Mass properties data are presented to describe the characteristics of an expendable second stage with a reusable space shuttle booster. The final mass characteristics of the vehicle configurations for three specified payloads are presented in terms of weight, center of gravity, and mass moments of inertia. Three basic subjects are the integrated vehicle system, the expendable second stage, and the booster modifications.
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Mass properties data are presented to describe the characteristics of an expendable second stage with a reusable space shuttle booster. The final mass characteristics of the vehicle configurations for three specified payloads are presented in terms of weight, center of gravity, and mass moments of inertia. Three basic subjects are the integrated vehicle system, the expendable second stage, and the booster modifications.
Key concepts: Booster (rocketry), Space Shuttle, Aerospace engineering, Inertia, Stage (stratigraphy), Environmental science, Computer science, Engineering