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Spacecraft Design and Launch Systems by Shubham Kumar is a document available to read on EtoBox.

The document discusses mission analysis for spacecraft. It describes how spacecraft must carry an atmosphere, provide protection from radiation, and only dissipate heat through radiation. It also discusses expendable launch vehicles, reusable launch vehicles, and the components of a space vehicle system including the spacecraft, launch vehicle, launch facility, and ground operation support systems. It further explains trajectories in space using gravity assists and Hohmann transfer orbits to minimize propel

Author
Shubham Kumar
Language
EN