Browsing Space Systems Design Lab (SSDL) by Subject "Aerodynamic characteristics"
Now showing items 1-1 of 1
-
A Conceptual Design for a SSTO Space Station Service Vehicle
(Georgia Institute of Technology, 1987-10)The objective of this research was to design a single-stage-to-orbit aerospace vehicle to service a U.S. space station. Several restrictions were placed on the design, such as minimum landing speed (165 knts.), stability ...