Design and Testing of a Vertical Take-Off and Landing UAV Optimized for Carrying a Hydrogen Fuel Cell with a Pressure Tank.

Autor:	De Wagter, Christophe, Remes, Bart, Ruisink, Rick, van Tienen, Freek, van der Horst, Erik
Předmět:	FUEL cells PROPELLERS PROTON exchange membrane fuel cells TEST design MICRO air vehicles TANKS FLIGHT testing EMAIL
Zdroj:	Unmanned Systems; Oct2020, Vol. 8 Issue 4, p279-285, 7p
Databáze:	Complementary Index
Externí odkaz:	Zobrazit plný text záznamu