Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011 2011
DOI: 10.1109/rast.2011.5966927
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Effect of atmosphere model on suborbital launch vehicle trajectory analysis for a hypothetical launch from Turkey

Abstract: There are several reference and standard atmosphere models which are claimed to be valid and accurate for different regions all over the world. Launchers, during their atmospheric flight, exposed to aerodynamic drag forces. Magnitude of these forces and trajectories of the launchers directly depend on the atmospheric conditions. It is a must to model the atmosphere accurately before the trajectory analysis in order to determine the trajectory of the vehicle precisely. Since there are no detailed atmospheric st… Show more

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