The hover performance of three full‐scale rotors was measured at the Ames Outdoor Aerodynamic Research Facility. The rotors. all designed for tilt‐rotor aircraft, were the original metal blades for the XV‐15 Tilt Rotor Research Aircraft, a set of composite, advanced technolongy blades for the XV‐15, and a 0.658‐scale model of the proposed V‐22A Osprey (JVX) rotor. The composite advanced technology blades for the XV‐15 were tested with several alternate blade root and blade tip configurations. This paper presents the performance of these three rotors, shows the effects of tip Mach number and root and tip configuration changes on rotor performance, and presents data on rotor wake velocity distributions and tip vortex geometry. Measured rotor performance is compared with theoretical predictions, and the discrepancies are discussed.