Browsing by Subject "hybrid"
Now showing items 1-4 of 4
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Design of a Hybrid Rocket / Inflatable Wing Uav
(Oklahoma State University, 2012-12-01)This paper discusses the design challenges and development of a UAV that transitions from a rocket, which allows the aircraft to reach a target altitude rapidly, and then deploys an inflatable wing from an enclosed shell ... -
Design, analysis, and integration of a turboelectric propulsion and power system for unmanned aircraft
(2020-05)Electrically powered small unmanned aerial systems face limited range and endurance due to the inherently low energy density of current level of technology batteries. Hybrid gas-electric systems are under development and ... -
Integration and power management of turbo-electric propulsion for multirotor UAV
(Oklahoma State University, 2021-04)The rapidly growing and continually evolving unmanned aircraft system market demands performance innovations in aircraft versatility, maneuverability, payload, range and endurance. Standard, fully electric designs with ...