In this paper, we will examine a configuration for a reusable military launch vehicle (RMLS) concept. This configuration allows for the vehicle to land in an inverted attitude. Such inverted landing improves the turnaround time of the vehicle by reducing the maintenance requirements of the vehicle's thermal protection system. An analysis is performed to examine the impacts by the configuration on stability, control, and footprint for an RMLS configuration.
Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle
2003
9 pages
Report
Keine Angabe
Englisch
Footprint calculation for a reusable launch vehicle based on dynamics programming
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